UIRTH, ZDLNEK, ed.
I
liatiborice; statni zarek a babiccino udoll. (,Ua-,rni stat napsal Zde,-2ek
Wirth. -'polupracovali: Gohumll Novak, et al. 'VYd- 3, v STI 1. V Fraze,
Statni telovychoviie nakl., 1955?) 28 p. (Ratiborlce; the state castle and
Grandinother(Is Valley. 3d ed. illus., maps)
SO: Monthly Index of East European Accossibns (EEAI) LC, Vol. 7, no. 5, &,* 1958
WIRTH ZDENEK
"Sychrov, statni zamek a okoli. (Titulovou stat napsal Zidenek Wirth. Spolupraco
Bohmmir Lifka at al. 2. rozirene vyd. V Praze, Sportovni a turisticke nakl., 1957)
P. 32 (Publikace Statni pamatkove spravy) (Sychrov, the dtate castle and its
surroundings; a tourist guide. 2d enl. ad. illus.., nap plans)
P. 32 (Praha, Czechoslovakia)
Monthly Index of East European Accessions (EFAI) LC, Vol. 7, No. 7, aly 1958
BROZKOVA, V.; WIRMOVA, Ii.; KUBAT, A., MUDr.; SYEIIIRA, J.
Our experience -wdth radioactive iodine ir. the diagnGsis af
thyropathies. Plzen. lek. sborn. 24:83-88 164
I. Klinlka chorob vnitmich lekarske fakulty University Kar-
lovy v Plzni (prednosta: prof. WDr. K. Bobek) a onkologicke
oddeleni SFN v Plzni (zast. prednosta: MUDr. Al.ois Kubat).
I
WISCII1U. H.J Dipl. Ing.; KULDA, V., inz. [translator)
Excitation of synchronous machines by rectifiers. El tech Gbl-:,r 5,3'
no.10:529-532 0 164.
1. VEB Elektroprojekt, Berlin, German Democratic Republic (for
Wischer).
WISGICKI, Marok
_T&Anological progress in welding. Wiad elektrotechn 31 no.12'.
293-296 D'63-
1. Zaklad Vytworezy AparatmT.'- :ii~idzielon6j A~!M& -Waromma.
WISILEWSKI -SWATEK) Stanislaw
--Llxdwik
Anodic decomposition of graphitized electrodes duringelectrol~sis.
Ft-.2. Sodium chlorate. Chemia stooow 5 ro.2t299-310 161.
1. Katedra Elektrochemii Technicznej i Elektrometalurgii, Politechnika
Slaska, Gliwice i Instytut Chemii Nieorganicznej, Gliwice.
SZR3WNR, Wald~rslaw; DZARNDCKI, Wilhelm; WISKOVf-BUCZKOVSK4,jWina,
JANICKI,Andreej ft%
Studies on liver-protecting substances. I. Observations on experi-
mental poisoning with carbon tetrachloride.. Pat.polska 6 no.l:
1-6 Jan-Mar '55.
1. Z Zakladu Patologli 0golnej A.M. w Gdauskm -Ueravnik: prof. dr,
W. Szreder I z Zakladi Anatomli Patol. A.M. w Gdansku. Kierownik
prof. Dr. W. C%arnocki. Adres: GkIansk. Zaklad Patologii Ogolnej i
Doswiadcsalnej, Debinki 7.
(CARBON TMRACHIORIDIC, poisoning,
exper.)
(POISONING, experimental.
carbon tetrachloride)
wIsKONT-BUGZKOWSU'Ah~'
exchange in hypoxic-hyp-ercaPuic hypothermia in rats. Acta physiol.
polow. 8 no-3:50-568 1957.
1. Z Z~kjadu yizjologii A 9 w Gdanaka. Kierownik: prof. dr B. Szabuniewicz.
(RISPIATION, Physiolous
eff. of bypothermias hypoxic-hypercapnic in rat (Pol))
(HYPO BXMIA. effects,
on gas exchange in rat, hypoxie-hypireapnic technic (Fol))
W'i -"na,
76 m
rg L. da Of Z n~-- c - L
dQ.:
J Oj
a F;:6 4 rio - il- Ag 63,
16 Z ~FrQOU F 1 ZJ Oll Og 1 J. P-k6(Nmi.1 :14eJyczrAej wMar Au 7 1 e rown'l~
wi cz).
prof dr. Szabunia
WISKONT-BUCZKOWSKA, Halina
1-1- --- -- - ..
Histamine metabolism in pregnancy and gestational activity
of progesterone. G-inek. Pol. 35 no.32439-"8 14y-Je 164
Histamine In human labor and pregnancy. lbid.2449-456
1. Z II Kliniki Poloznict,,ra i Chorob Kobiecych Akademii
Medycznej w Gdansku (KierownikI., prof. dr. med. R.Gromadzki).
PAPIFIROUSKI, ~'bignisw
Comparison of results of 1=.jrologic pregnancy test
no.4-423-427 Ar, 165-
Pichheim-7cndeck test. Gi.neks Pole 36
1. Z II KIJ.niki Polomict-wa i Chorob Kobiecych AIIA w Gd4rw;kLj
(aerownik: Prof. dr. med. We Gronadzki).
peal
ratows beefilk"
wo
lius. The 11"M tally, Isably
%ihofoiaft ~- I'll ~ C~Anmfgcwllmi Wily
locim- lie
,
viry S the Gerumns-
Ivy I-Pin
Stefisn, mgr Inz.; URBANlKI, (Ir
%he position of
Analysis cf modern r~&.thcd3 of
-L 4 -1 gec-d 35 361 no. 32
a Ohip at sea. Pt- 2- 1'rza,
9P,-Iol Mr 164.
WISLA, Stefan mgr inz.
Terminology in the field of maritime hydrography and its tasks.
Friegl good-34 no.10:422-425 0 '62-
..WISIA,.,Ste mgr. inz.; 7irbanskij, Jozef, dr-
Analysis of modern methods of determining the position of
a ship at sea. Przegl. geod. 36 no.2t57-.60 F164
-...L-4,1032-66. 13C
ACC NRt AP6 SOURCE CODE% PO/0082/66/000/002/00,
AUTHOR: WIslaq S. (Mader engineer.' Lieutenant)
ORG: none
TITLE: A simplified method of determining the accuracy of a ship's P081#1on plot,
SOURCE: Przeglad moreld, no. 2,, 1966, 64-73
&6~
TOPIC TAGS: phip navigation celestial navigation, navigation aid
ABSTRACT: Analyzed are evaluations of average error M in ship's position plots calculated
from two or three reference lines. The author presents several tables and a nomogram assist-,
Ing In rapid determination of M for calculations with two or three reference lines derived from:
sightings, radiolocation, distance, or height of celestial bodies. The technique of using the 1
cited tables and chart Is Illustrated by several practical examples. Calculation time Is about J!
1 min and the results insure adequate accuracy of the plot. Orig. art. has: I figm, 3 tables,
and 7 formulas.
SUB CODE: 17/ SUBM DATE: none/ ORIG REF: 004
IfEBSKIp Marian; WISLAWSKA, Barbara
A case of parathyroid adenoma with..signs of Recklinghausen's
disease and severe anemia. Fol. tyg. lek. 17 no.5:182-184 29
Ja-162.
1. Z II Kliniki Chorob, Wewnetrznych AM w Lodzi; kierowrdk: prof. dr
med. Jerzy Jakobowski. I
(OSTEITIS FIBROSA compl) (ANEMIA HYPOCHROMIC etiol)
IZDEBSKI, Marian; WISLA14SKA Barbara-__
Acute allegic toxic syndrome fo3-lowing meprobamate (miltOW09 P4DI-
tyg. lek. 17 no .10:363-364 5 Mr '62,
1. Z II Kliniki Chorob Wewnetrznych AM w Lodzi, kierownik: prof. dr
nauk med. Jerzy Jakabowski.
(MEPROBAKATE toxicol) (ALLERGY)
g g=,,g:!jj)g
'g vg
F: WW
MINOR OWN Hill I'l IN I, I
WISLAWSKI, Jerzy, WOLTM, Halina
Temporal arteritis. Neur. &c.polska 5 no-3:27?-285 My-Je 155.
1. Z Kliniki Neumbirurgii A.M. w Wareumle. lierownik: -prof.
dr J. Chorobaki. i z Kliniki Okulietyczuej A.M. w Warssawie.
Kierou-nik: prof. dr W.H. Nelanovski.
(ARTMTIS
temporal, clin. aspects)
KOZNIEWSKA, H.; WISLAWSKI,J; SLOWIK,T.
Epidermoid cyst of the spinal cord. Neur. &c polska 10 no.2:213-217
mr-Ap 6o.
1 Z Kliniki Neurochirurgii A.M. w Warszawie Kierownik: prof. dr med.
J:Chorobski.
(SPINAL CORD neopl)
KEPSKI, Apolinary; WISLAWSKI, Jer2y
Case of total blocking of Magendie's foramen in an adult. Nseurol.
neurochir. psychiat. pol. 12 no.6:925~-928 162.
la Z Kliniki Nourochirurgii.AM w Warazawic Kierownik: prof. dr
J. Chorobski.
(ITEUROLOGY)
Clinic
-Uto
'IT'd ep.
.1i -e
&demiii tied
r S !I'! pi'lontdalis)."
F coree,
'
4:1 c t I~ft,2; pp 11579=1611.
10
7 male and I fw4 1e
Clinicp
,I datp on I r., p 'th,
sual suraica
tvc&ted by tbe u
t5 oF whom v e.
6
V q4k'~S
~1, Jerzy; MAZUROWSKI, Witold; LEWICKI, Zdzislaw
Metastatic tumors of the brain. Nowo-twory 14 no.3,253-257
Ag-S 164.
1. Z Kliniki Neurochirurgii Akademii Medycznej w Warazawle
(Kierownik; prof. dr. med. L. Stepien) i z Zakladu Anatomli
Patologicznej Akademii Medycznej w Warszawie (Kierownikt
.doc. dr. med. R. Stanczykowa).
WISLAMSKI,_,~erzy,;, JTIAFTEK, Jan; ZARSMI, Stefan
Co-existing 2 cerebral tLunors originating from different embryoniL-
formations. Pol. tyg. lek. 19 no.30:1165-1166 Z7 J1164
1 1. Z.Kliniki Neurochirurgii Akademii Medycznaj w Varnawie;
kierownik: prof. dr. med. Ijicjan Stepieno
JISL9491 M
"Interesting ideas on resin collectiezell p. 24 (Jas nojakj~ Vol. 26, No. 2, Feb. 1952,
Warszawa)
East European Vol. 3, No. 3
SO,s MoAh LiBt of Accessionsi/Library of Congreasp March 1951., Uncl.
WMIAWSKIS M.
WISIAW9KI., M. Sinplified method resinifying spruce* p9 Be
Vol. 29, no. 10, Oct. 1955
IAS.,POLSKI
AGRICULTUM
mcchAn
PP- 314-319, 2 fjR,,. LWJ"" Pl~;914d BudowIsny. No. ?__S.
"lepixing the definition,
M"h&nfZlktlon of worof b"', "Ifthankation Index And .Ingle
Ournparally, . k. XXIIIAnAtion. on
Of [tie ba'SIC me nalyals 't both Indices And the b4al, of exit -X of
Indkv. In pla,lell"'llizatiln In 'he cOmequent a gripir"
IhOdf by Meallm ning. An pygM dox AS one of the MAI doption
nf th rimmi. to n find fundamuqtAl
lplnnt r 111('11antitalln Interlink Ill. pj4nllbjjt
14tes 141141 "I'llimmne indkrx . d
tie Caro-Ing fill( 77he doterni, it by Mralul nf tj*
t
viring In building A More throuch na,,'n * this link
CCU of M" PrActke in Analyalm of the, features ft-
'hanization ronjuell.
wilth the proXce"
"Itic Of bulc Mach 1,,rDetertnination of th Agnitude In the IWO.
Y,. 0 in w the
required for ;he mechanlf-f* "Unit
.he fun-
Immo
L
62t.96/
lish Teohnical Abstracts
P 9 r planned Per-IndIc Preventive- Overhatils rl
teni 0
S
o
1953
No
4
rs
. Th
;NVIJII At 'd 11Y
ns , Advance
1 1jamy Plant, According, to sugXesti
t
.
,
d ,
ra
Con r~l
On
Con
'
:
C
Building Industry an the 10, in
"t6w elq~
.
eh z3poblegawczych rPmN
l
Architecture nOwY
"SY4:.:= Pla~:)%va-term
h W!dtug PrOJelctu 1OX31%. prieglAd Suda
Mjs,yn bulawlinyc
'
kich -
31r__318.4 tabs.
&' 195,~ p~.
0.
wiany. N be carried out, In a*system of P12r'-,t,.i eco
lant should
RapILM to p
The sYAtem Ad0D't!d In Pa-
ce,)rd3nee with a datalled Plan.
l
i
I
n a
nomyt
A sys'wn Of Plknne~l p-2r-j
eve-Itive overhaul-
~
i3nnezi pr
land relle3 On p
.o. cl6sely the Ir'tPrvCnI.1g
ked out 4.0 define
tic overh3uls ha3 been
ooliod bitween such
Polish Technical Abstracts
4t 1953
No Foudallo"S for the PRIMOU of c(Illurt an,l sclell,e,
Building Industry and Oudowi fund,,,,,-nt6,,
I I Pr7,cglld Dii.
dowtany. Na, 10. 1932, Pp- 30-38j, 11 figs.
Arohitecture
0foundations for the highest pirt of the Palac3 of Culture and
Science form a 7-metre high reinforoed co'ncrete box rcughly -to
n, ua area. The foun:Wlon Plate *Of' tile re!nforccj X 70
r
co
0:1-a, concre*.e I)-L5C. MOre than lo cantl co:I,Crptc L-,JX
L~
L"'d 'mn
iram--dLa'ely on the bottom
ld of 4he exca re!
verUcal baulaga of ma. VaLlon. Horl
erlais was effectei~-:?--- --mi-O,Fhc--vY cranes
hO's
I L.:V ~6. Vie reInforcament was carried out in the forn, .( gr,ds
Aad la 1, 5 moasurlag~-.P-to 66 -,q- The shutteriig f,-~r ti,
was -Iff-- fgrm 2 Mrnerele
the
w7 r
e~ d ovej again. of large P'ates and angles, capable of %cing
v
U~ed Ov r an
3056 93A5:7nM
j, Production of Large Prefabricaied Cellfec Slabs at the
J. %tallm Memorial Palace of Culture and Science..
,,Produkcja wielkich ptefabrykowanych plyt gtropowych mi bu-
dowle Palact- Kultury t Nsuki Im. J. Staltna". PriRglqd Budowlany.
No. 8, 14
, ", pp. " M4)-26 1, 4 figs., I tab.
Prefabricated slabs ar- being used in conistruction of cetlings not
d-igned for h-rizontal sUffening. The slabs are made In special mnutd-%.
nctually, on the building site. As a rule, steam curing of the stab$ takes
23 hours, which I.-; adequate to produce a strength of R = 0,75 Rf~4.
Given proDer production organigatlart, correct design of th,- glabs and
01.- 1- ~f ".-, -.:-t- f .-h
1IMPIC
WISLICKI, A.
(INZYNIERIA I BUDOWNICTWO, Bol. 10, No. 11, Nov. 1953, Warszawa, Poland)
"The industrialization of work on the building site of the Stalin Place of
Culture ard Science in Warsaw,* P. 330
SO: MONTHLY LIST OF EAST EUROPEAN ACCESSIONS, L.C., Vol. 3. No. 4, APRIL 1954
WISLICKI,A.
ItConcrete Work On The Bu4 Min - Site --Of The- Palace Of- Culture And Science" P. 11.
(Przeglad M Vol, 25, no, l.-Jan& 1953, Warszawa)
East European Vol- 3. No.2,
SO: Month List of 1=32= AccessionsY /Library of Congress, Februar7, 1954 1993:, Uncl.
I&TSLICKT; A. ure And
ssembling The Steel Frame.of-The Palace Of Cult
~y rszawa)
WISLIC j p,. I yOVIAWZYK) - R. "A 1953, Wa
=L . -Vol. 25,, no. 3j. Mar
Science :[n Warsaw" p. 67- (Prze lad-BudOulany
Fast Europpan Vol* 3j No., 2; as, FebruarY., 1954 "U.,.Uncl-
a= Accessionsi/LibrarY of COngre
so'. tMth List Of/Xu
rf "-e C,~,'rl
-.-rlks ";flz;cll cn, the
;,-rial cent-cros;
cc
aL tho Pala
zawa, Pollard)
jql,~, Wars
0.12, Dec*
1101 3,
so: KontblY List of East Phuro-11-C-M-1 C~,Cces:3io-,S,
1954, Uncl.
'
T
JISLici-I, A.
110-reanIzati(,n in lbuilding 7,rilaf--r -f,
Warsaw" (,-ID-`]GIdUl fit,ki AIN, Vol.
ib. 10, Cdolvr 3.954, 'larsaw,
Poland)
SO: - Yonthly List cT East Furopean Accessions (TT--,AL)j I,C~ Vc!, 4, 10. 3;
Mareh 1955, Uncl.
WISLICKI, A.
"Winter work on the conetruction of the 1. Stalin Palace of Ciilture and
Science In Waraqw." P. 377. (PUZErIGLAD BUDOWLM. Vol. 26, No. 12, Dec. 1954
Warozawa, Poland)
SO: Monthly List of Bast B"dpean Accessions. (EFAL). Lo. Vol. 4, No. 4.
April 1955. Uncl.
WISLICKI, A.
"Horizontal, Trarmport in the Construction of the Hi_,7hesf- Parts of 4.r:--
Stalin Palace of Science and Culture in Warsaw#" P.54. (PRZWLAD MRIMNY
Vol. 75, No. 2, Feb. 1954. Warszawa, Poland)
30; Month3,y List of East European Accessions, (EEAL), LC, Vol. 4,
No. 1, Jan. 1955 Unel.
WISLICKI, A.
Influence of the Palace of Culture and Science on technical progress in
Polish building. p. 110. Vol. 12, no. 4, Apr. 1955. IN M IRRIA I BLUMUCTWO.
Warszawa.
Source: East European Accessions List (EEAL), IC, Vol. 5., no. 3., March 1956.
300-December 7,
vol. 2, Feb. 19515,
Monthly UA !)f -I U', Vol. 4, "'X-Y
art j,,Uj-ot(,,ajj pcce,~isir-in.5,
195~,, Uncl.
The Greeks were not only great architects but also building managers, P. 82.
(PRZEGLAD BUDOWLANY, Warszawa, Vol. 27, no. 3., Mar. 1955-)
SOt 'Monthly List of East European Accessions., (EEAL), LC, Vol. h, No. '61 4~ 1955,
Uncl.
TWISLICKI, A.
Pumping mortar. p. 121.
Vol 27, no. 4,- Apr. 1955. PRZE-GIAD BUDOWU'T'I. Warsaw, Poland.
So: Eastern European Accession. Vol 5, no. 4, April-1956
ItrISLICKI,_A.
The opening of Stalin's Palace of Culture and Sciences in Warsaw. p. 233
PRZEGLAD BUDMILANY
Warsz&wE-
Vol. 27, no. 7, July 1955
SOURCE: Ealit European Accessions List (ERAL), LC, Vol,/5, no. 3, March 1956
WISLICKT, A.
Development of mechanized h1lildin.q and its- iniustrializa,lion P. 32.
Vol. 4, no. 1, Jan. 1956
POZEIIIII STAVBY
Praha, Czechoslovakia
Source: Last European Accession List. Librery of Conigm-ass
Vol. 5, I-To. 8, August 1956
WISLICKIP A.
WISLICKI, A.
Trends in the development of rechanizatIon and the production of
buildinp raebinerr. p. 29
Vol. 5, no. 10, Oct. 1956
BUDOWNICTWO FRIZEFS1 (Y;,~E
FOI ITICAL SCIENCE ,
Warsiawa, Poland.
So: East Eurorean accession Vol. 6, No. 3, March 1957
WISLICKIp A.
WIS-LICK-Iq A. Mechanizing the building industry. p. 128
Vol. 28P no.3, Mar. 1956
..PRZEGLAD BUDaiLM
TECHNOL40GY
Warazavap Poland
So: East European A ccession,, Vol. 6. no. 2. 1957
WISLICK11 A.
WISLICKI, A. More attention to historic remnants of technique. p. 198.
Vol. 77, no. 5, MaY 1956
PRZEGLAD TECHNICZNY
PHILOSOPHY & RELIGION
Warszawa, Poland
SO! East European Accession, Vol. 6, March 1957
WISLICKI, A.
"Today and tomorrow of the Museum of Technology of the Central Technical
Organization."
P. 101 (Przeglad Techniczny) Vol. 70., no. 3, Feb. 1958
Warsaw, Poland
SO: Monthly Index of East European Accessions (EEAI) LG. Vol. 7, no, 4,
April 1958
WISLIC KI, A
TECHNOLCGY
Periodicals: PRZEGLAD BUD%MANY'f Vol. 30Y no. 7, July 1958
WISLICI~T-, A.. Comparison of the mechanization of the construction industry in
the USSIR, the United States, the German Federal RepublIc., and Poland. p.261.
Monthly List of East European Accessions (IYAI) IC, Vol. 8, Fo. 2,,,
February 1959, Unclass.
WISLICK-T. Alfred, doc. inz.
Mechanization of finishing works. PrzegI budcrr-11 i Imd --iasmk.
23 no.80-13-514 Ag'61.
HIM
WISLICKI, Alfred (Warszawa)
Testing thd usefulness of new types of building machines.
Prhegl budowl i bud mieszk 33 no.7413-415 JI 161
WISLICKI, Alfred (Warszawa)
Dynmnics of the development of building m-echamizatirn. P--Zegl
budowl 34 no.3:151-159 Mr 162.
1. Czlonek Kamitetii Redakcyjnego miesiecznika "Przeglad Budo-vilany."
WISLICKI: Alfred, doe., -Marlp inz. (Warsaw)
Dynamice of thO devolopmnt of builAing industr7 mchanization*
: I*ohanizace noo9:108-12.1 162.'
Ins stavby 10 no.9:Suppl
WISLICKI, Alfred., doc., inz. (Varsava); TOTH, Ladislav, inz. (translator]
Efficiency of building machilras and their manufacture in
various countries. Inz stavby 10 no.UsSuppl.04dchanizaca
no.lltl3l-134 162.
1. SNR, Bratislava (for Toth).
X
WISLICKI, Alfred (Warszawa)
~-~~~Once Fg~the need of educating mechanical engineers for
1
the building industry. FrzegI Vudowl i bud Mie3ZLC 34 n0-9:473--
474 Ag 162.
DZWONKCWSKI,'Kazimierz (Warszawa); KOZIITSKI, Wieslaw (Warszawa);
WISLICKI qf;m~=aiW -
-
Mechanization of finishing works. Przegl budowl i bud
mieszk 34 no-9:544-548 S 162*
W
WISLICJU -,-Altreds doe* inze,
Methods of determining the usefulaeoo of construction machiner7.
Przegl budowl i bud mieszk 35 no.lt65-68 Ja f63o
WISLICKI,'Al~red; MOLIVSKI, Roman
The state of equipment supply at constructior works in Warsaw and
ways to improva tho situation, Przagl budowl i bud mieszk 35 no,9;
483-485 163.
0
0
WISLICKI. Alfred,._doc. inz.
Operational testing of the aptitude of earthwork
machines in Poland. Inz stavby 12 no. 2: Supplement:
Mechanizace. no. 2: 17-20 164.
1. Ustav organ12ace a mechanizace stavebnictvi, Varsava.
BRACH, Ignacy; ROjEK, Karol; yjpjjqKj,_,.Alfred (Warszawa)
International Conferenci'on Mchoknization in Earth-dor1k. Przegl budowl
i bud mieszk 36 no.3:1506~1-51 14* '64-
WISLICKI, Bogdan
On the possibilities of increasing the combustion heat of
hydrocarbon fuels. Przam chem 39 no.51240-244 MY 160.
Ir
P1101 204~7
D227/D305 04P/005/001/002
AUTHOR:
TITLE: Increasing the heat of combustion of hydrocarbon fuels
PERIODICAL: PrzemysR: chemiczny, v. 40, no. 5, 1961, 240-244
TEXT: This is a discussion on the possibilities of improving jet
ai-rcraft fuels by adjusting the hydrocarbon combustion and by us-
ing B, Be, Mg, Al or their derivatives. Heat given out by a fuel
can be increased by incorporating components possessing high heats
of combustion. This is the fundamental criterion of fuel quality,
depending only on the-ililtial mixture and..products of combusti-on.
Complete,oxidation of C and H gives:
I KgC + Kgo Ll Kg CO + 8140 Kcal
2 2
1 KgH + 8 Kgo 9 Kg H 0(steam) + 28800 Kcal. (2)
2 2 2
Card 1/19
20437
-P/014/61/040/005/001/002
Increasing the heat of D227/D305
From the percentage amounts of carbon (c) and hydrogen (h) in a
particular compound, the heat given out in combustion is given by:
Qd = 81.4 C + 288 h Kcal/Yg = 'lower' calorific value (3)
and
Ag = 81.4 c + 341 h Kcal/Kg = heat of combustion ('upper'
calorific value). (4)
For jet and turbine engines, combustion heat is the most important
fuel property, since this determines the exhaust velocity of air
and, hence, the thrust. For compounds containing oxygen, Eqs. (3)
and (4) become:
0
Qd = 81.4 c + 288 (h Kcal/Kg (5)
Qg = 81.4 c + 341, (hl- Kcal/Kg. (6)
Jet fuels are chiefly derived from distillation and d-wzical treat-
ment of petroleum and coalta~. In the USA 1.39 5.6 and 18 million
Card 2/19
20107
P/014/617d4O/OO5/001/002
Increasing the heat of ... D227/D305
tons were produced in 1950, 1954 and 1958 respectively and produc-
tion is expected to reach 30 million tons in 1964. (Ref. 3: Reak-
tivnoye toplivo USA, Moskva, 1956); (Ref. 4: Petroleum Proc., 10,
343v 1955); (Ref. 5: World Petrol, 28, no. 11, 55, 1957); and
according to E. Bass, J. Lubbock, C. Williams (Ref. 8: Proceedings
of the Third World Petroleum Congress, section VII, Leiden). Total
heat evolved in burning is the sum of the individual heats of com-
bustion, 40 % of the energy being due to H and 60 % to C which
constitutes 84 % of the fuel by weight. Calorific values of various
hydrocarbons containing equal amounts of C are shown in Table 1,
while those for a number of homologous hydrocarbon series of inter-
est are contained in Table 2. CCalorific values of hydrocarbons may
be discussed in terms of the . ratio which forthe fuels in question
varies from 5.7 to 6.7 with corresponding Qd values of 1-0,000
109500 Kcals/Kg, and in connection with the boiling points, since
these determine which compounds will be associated in a given
fraction during manufacture (Figs. 2 and 3). The value of (Q g_Qd)
Card 3/19
2C437
P/014/61/040/005/001/002
Increasing the heat of ... D227/D305
is 770-800 Kcals/Kg for alkanes, 750-770 for alicyclics and olefins
and r\j38O for benzene homologues. Calorific values and H-content
of alkanes fall with increasing b.p. For single-ring alicyclics
Qd is little affected by the b.p. and it increases in higher homo-
logues of the benzene series due to the H-rich side-chains. NaDh-
thalene homologues have lower calorific values than benzene, eg.
n-Bu benzene 99459 Bu-naphthalene 9P535 Kcal/Kg. The calorific va-
lue per liter Q, (= Qd - x density) is more sensitive to chemical
composition than Qd (Table 3). A few examples are quoted showing
that Q, of alkanes, cycloalkanes and alkenes changes appreciably
with the structure of the carbon skeleton. For the aromatics Qg de-
creases and Q1 increases on addition of an aromatic ring with a
1-2 carbon side-chain. The thermal efficiency of fuels can, there-
fore, be increased by including compounds of high Qg and densityg
bearing in mind the composition and b.p. considerations. Thus the
Card 4/19
F,101 204 7
4/61Y~40/005/001/002
Increasing the heat of ... D227/ '305
calorific value of jet fuels (lo,250-10,350 Kcal/Kg) may be raised
to 10,400-10,500 Kcal/Kg by using a parafin/olefin mixture of den-
sity ~-iO.77. Raising this value to 10,500-10,600 with fuel densi-
ty > 0.77 is considerably more difficult. Fuel usefulness also de-
pends on the melting point, viscosity, corrosion characteristics,
vapor pressure, inflammability, rate of combustion, frame stabili-
ty, coking tendency, engine design etc. ZIbstractor's note: These
factors are not discussed7. The calorific values for a number of
fuels are given in Table-4. Certain metals and non-metals and
their compounds are otentially useful fuels because of their high
heats of dombustion Uable 5). The usefulness of these elements is
assessed by means of a "fuel index" X, defined by
X Qvol' (7)
0 0
Kt , Qvol
where Qwt and Qvol are the calorific values of the material tested,
0
per Yg and per liter respectively, and Q S are the corresponding
Card 5/19
20437
P/014/61/040/00r-1/001/002
increasing the heat of D227/D305
values,for paraffin oil 0 0 109280 - 89540 = 87.8 - 10 6
Kt 0 Qvol =
Values of X for certain materials of interest are listed in Fig. 4.
Use of hydrogen which possesses the highest heat of combustion is
deterred by its unfavorable physical properties. In the search for
better fuels (1): Be and B can be usefully substituted for C in a
hydrocarbon molecule or, alternatively, (2): Suspensions or colloi-
dal solutions of metallic powders in hydrocarbons could be employed
(1): Interest in B and its compounds has grown recently, although
its.physico/chemical properties have not as yet been fully investi-
gated. Boron hydrides with calorific values > 15,000 Kcal/Kg are
of particular interest. Certain properties of these and related
compounds are shown in Tables 6 and 7. (2): Suspensions are pre-
ferable to colloidal solutions, where the achievment of high con-
centrations presents serious difficulties. Life of the suspensions
may be prolonged by increasing the hydrocarbon-viscosity and by
stirring, Physical characteristics of A120 3 p B203 , BeO, Li2o' 14go
should also be considered since they may absorb considerable heat
Card 6/19
20437
11040100510011002
P/O 14/
i.ncreasing the heat of D227/D305
in melting or even vaporizing, and being solids, will accelerate
both.erosion and corrosion of engine parts. Recent American work
on boron and its derivatives for us6 as aircraft and rocket fuel
is briefl mentioned. The author considers that at present -the use
of Al(BI-1 Li and 3 hydrides.allows a.50 0 increatie in engine
4 3
thrust. As an illustration, the maximum flying distances of a 58
ton plane with 125 m3 tanks are quoted as 16,000-35,000 kin for the
above mentioned metals, hydrides and metal suspensions as opposed
to 14,500-15,000 kin of the conventional fue Is (15,000 for kerosene).
There are 4 figures, 8 tables and 28 references: 11 Soviet bloc
and 17 non-Soviet-bloc. References to the four most recent English-
language publications read as follows: H. Harvey, World Petrol,
26, no. 10, 54, 1957; H. Harvey, SAE. J. VIII, 65, no.9, 17, 1957;
I.R. Cracknell, Plight, 71, no. 2512, 332, 1957; Ind. Eng. Chem.,
.49, 1265t 1957.
Card 7/19
P101 2 37
4/6 1%4 0/005/001/002
!. ~Increasing the heat of ... D227/D305
Table 1. Oompoeition and value ST,blla,l, Wartodd O~;Io'W'**Orsx Wad Slementarny rdinych
of various
hydrocarbons. 'rAtLF
Igrup wqg1owodordwd)
egend: 1
Hydrocarbon; 2
qslowod6r
2
6r
SkIAd eleme~tarny Wartold
GO Palowa
kcal/kG
-
formula; 3 - composition; H, -1. C. -I. TI
t01.. J 'Og6rna
4 - calori fic value, kcal/kg; Ufeksn ql~'
I q
g
1: 83.74 M98 11560
5 - lower;
6 - upper; 7 - he- k... .
Zne ,
, ~"': a
1
~
85.72
20615
'1".
xane; 8 -h
exene; 9 cyclohe- k1oheknn QUIS
11
C 14,28
7
60 83'n
92
31 10379
9533 11150
16H0
xane; 10 benzene. 0
4
,
,
Table 1.
Card.8/19
20437
111014Z61100100510011002
j -icreasing the heat of ... D227/D305
Table 2. Distribution of the
calorific value in homologous
series.
rmAr 2-
T a b I I c a 2. Hoskind Warto1c) OPRJOW#j W Arzeregach homologfrx-
Series; 2 - lower
Legend: 1 VC111PT),
calorific value (kcal/Kg); Wortold ot)Alown dolnA kcal/kO
n-alkanes; 4 - iso-alkanes; Smell homoloalmy
5 R-olefins; 6 - -s-117gle-ring C.
alic7yelice; 7 - double-ring ali-
No-41a
Paraliny ID is"s 10570 10540 1f"3
cyclics; 8 benzene and homo- frop4rallay 40
Normalne ole(Iny 0
1"15 IZ33
10163 30513
10470 Mll
101,64
logous; 9 naphthalene homolo-
0
kl
11M
16"s
IWO
gous; 10 - aromatic-cyclopara- o
ey
Dwilplericleillowt
ffin hydrocarbons., Q0
Dowell I jtgo hams.
5393 "AS "17 -
ITOM010KI nattalenu(i) - 9"1 105 -
WQitlO%VO(lGTY
Table 2.
t yet iie-eyk lops rA fl.j
ltUW#
Card 9/19
20437
Increa
the heat of
in P/014/61/0
D227
D305 40/005/001/002
s
g /
Table 3. 'Calorific values per : T a b I i ca3WartodA opalowe z kRograrns I z 11tra iwi4xk6w
+'kg and per liter for various priedstawisjqcych Poswre961ne szeregi hoinalogtezried) 1 416LE
compounds representing parti- 0 ~3)
';"We
cular homologous series. Wqgtowod6r W~lr d.-
I
keel/kC ~fj
kcalil
Legend: 1 - Hydrocarbon; (D n-Efekan.
0 De C.H.
C
H 8,7bg
0
7ft IN70
18183 7080
7740
20 cen-2 .
W l
,
2 - formula; 3 - density (d Butyloeyk1ohekson
O Cjr- 9.7M lam am
4
4 - calorifid values; (BDekaUna (trans) CwHp 6.872 10165 rM
5 - kcal/Y
6 kcal
A GDekaHna (cis)
-I)But
(1
lob C.U1,
11
q 0,890
0
3 10225
9M 9100
M
g;
7 - n-decane; 8 decene-2; -
enzen
y
C.,retraiins, .
1.
I.C~.H.' ,VA
S.Sq3t V23 9450
.9 - butyl cyclohexane; Gmetylonaftatien q.H. 1.025 92*4 961-5
GNafta lotnicza (11rc) IMSO 8300
10 - trans-decalin; 11 - cis-
decalln ; 12 - butyl'benzene-,
13 - te tralin; 14 - methyl naph-
thalene; 15 kerosene.
A
.J Card 10/19-
increasing the heat of ...
Table. 4. Calorific values of
fuels and the constituent hydro-
carbon groups.
Legend: 1 - Fuel; 2 density,
15-0/15.50; 3 - boiling point,
OC; 4 - group composition, %;
5 - calorific value; 6 - aroma-
ties; 7 - cycloparaffins;
8 alkanes; 9 kcal/Kg;
10 kcal/1; 11 aviation fuel;
12 kerosene; 13 - alkane con-
centrate; 14 - alkane/alicyclics
concentrate; 15 - aromatics con-
centrate; 16 - aviation spirit;
17 - diesel fuel.
4
; .
;
Card 11/19
P/01 416 ?W4'9/005/001/002
a b I i*~~ "WahM Cl'opafowe Pal1w I Frup woglowodordw weho-
dzqcych iw Qclad Pallwa)
(D "
.
T
a Sklad grupowy
1A. Warto9k
~opalowa
Pallwo D
W. Aro- Maps- Ik' Ll I licit
M Rty- raft. rall-
CInO
r1owe
kG
I
nowe
Aliwo lotnt-
Yeze 01765i 60-270 - - - 10150 TOO
,N&fta lotnicu 0,7910 155-"0 19.4 39.2 41,4 IOUG 8135
~C..cent,.t
)-,jwqglowodo-
r6w parall-
nowych 0,7475 159-265 2.6 3.2 97.2 10,10 "23
?ComentrAt
I wqK10wodo-
JA r6w parafl-
'-'
nowych I c7-
klopjlraflno-
~!
Wych 0,7010 100 -274 1,4 51,9 40,7 10100 1133
Koncentrat
e~,WqKlowodo-
r6w aroma-
lycznych O,e545 156-253 75.2 11.4 13,4 SS60 -0
n yna lot-
"
1C
.1
CZ3
0,7103 50-1"
1
faltwo do all-
nik6w diesia Q.tIOG -1 10058 8?20
Increasing the heat of ...
Table 5. Heats of oombustion
-ce tain
of r substances.
legend: 1 - Aluminum; 2 - pe-
trol; 3 - beryllium; 4 - magne-
sium; 5 - -hydrogen; 6 - silicon;
7 - acetylene; 8 - titanium; 9 -
lithium; 40 - lithium hydride;
11 - carbon; 12 kerosene (pa-
raffin oil); 13 boron; 14
tetrahydro
diborane, B2H6; 15
borane, B2H6; 16 - pentaborane,
B5119; 17 - decaborane BjoH14;
18 - suspension of B in kerosene
19 - suspension of B in pentabo-
rane; 20 - AL 140 atm.absolute
(above 1 atm) and 1 OOC; 21 - AL
350C; 22 - AL 9900; 23 - aub-
stance; 24 heat of combustion;
Card.12/19
20h-37-
P/014/61/040/005/001/002
D2 27/D305
03 Clew 59412MI&
W,
w iq
Sto Un k
fl
Substanell d
12'r OM .
charak
haty ftbity rystymny
kcal/l (d1s nat- (dia nat-
ty - 1) ty - 1)
Mn 28043 2,U 7400 0.12 1.71
3enzyna 7280 0.85 104" 1.01 a."
cry' 29950 3.31 111" 1.57 5,40
agnez 10300 1.21
P, 5933 0.51 0,70
Yod6r al 9-
0,04 2we 2,70 1.05
c,--- i7ece 2," 7330 0.71 1.47
tcetylen 7150 0." 11520 1.12 0.2
1
ryton
:0520
2.40 4350 0,44 ,
1.0
~,t 5170
:,
: 10265
1 3,00 2.63
Nodorek litu
8060 3
:
9050 0.93 a,"
11520 2,01 1830 0.75 1,59
qatta IS40 1,00 10290 1.00 1.00
Br 32100 3,76 1"30 1,34 5,17
"w"O"w"dr ,
132114 T705 Oil 17436 1.10 1.57
picrohydrobo-
rowod6r 82110 93W0 1.10 19700 1,11 1.78
riqc1oborawo-
'
d6r BsHe 9876 1.13 16110 1.58 1.83
resiqclobor-
C~5
1
wod6r BlaH14
13250000) &,85
14400
1,40 1
1
1.91
~awlestna boru
w nafele 20500 3.40 12"G 1.25 3.10
wlestna boru
a
~
w BSHq
21350 2.50
14400
1.40 '
20437
P/014/61/040/005/0011/002
Increasing the heat of ... D227/D305
1e 5. (cont'd)
Tab
25 - kcals per liter; 26 - relative to paraffin oil (paraffin oil
- 1); 27 kcals per kg; 28 relative to paraffin oil (paraffin
oil 1); 29 - fuel index.
Table 6. Characteristics of some boron hydrides.
legend: 1 Compound; 2 - formula; 3 melting point (0C); 4
boiling point (0C); 5 spec. gravity; 6 - vapor pressure; 7 gen.
properties; 8 - stable pentaborane; 9 decaborane; 10 - borazole;
11 - aluminum borohydride; .12 - beryllium borohydride; 13 - lithitn
borohydride; 14 - not decomposed in air between 0-100C. Slowly hy-
drolyzed by water; 15 - does not ignite or decompose, slowly hydro-
lyzed; 16 - chemically stable, soluble in water? not hydrolyzed in
the cold; 17 violent reaction with air and water; 18 - violent
reaction with air and water; 19 stable in moist oxygen.
Card 13/19
Increasing the heat of
Table 6. (cont'd)
T a b I I c to 0. Churn ktorystyka n1ektdrych borowallar dw 0. to- 11.
107, 1. r. Q
Temp.C) -remp.
Zwlqtck 6r wrz.
,c
Plqctoborowod6r
trwaly (15,1 przy II
DzieACcloboro-
99,5 I
213
wod6r (156 przy 162
B.N.U.
130row0doro-
Horowodorek jillnu Al
Uorowodnrek be. Be
rylu
Borowodorek litu L--i7i-
Card 14:/19
2007
P/01 4/61/040/005/001/002
D227/D305
CD Clqtar Pr4tt m Winsnold og61ne
Nlnieiwy per
0,610 Gatio.) nle, rozklada siq na pu--
mm) W) awletexu w 0 do 10'. "1
dzialantem H--O ulega Do-
wolnemu rozkladowt
0.92
1 19 (low) We Zoppla Sig* nie Illega
mm) (99
) r.zktndwA . ulga Onwol-
nel hydroUxle
53 0,8519 chemiante trwaly. ruzpla-
szczalny w H-0 bez roz-
kladu. nrzy ogrzanlu hy-
-
- drolizuJe
-
(Bit.). -6314 .44,3 0,3508 1 FS
(I-) 9waltownle rengule z HzO
(t3. I Dowletriefp
(DIIJ, 31 91p jak WYtej
237 0,668 trwaly w atmosferze tle-
P
nu I wilgod
20437
11/014/61/040/oor.-,/ool/002
ncreasing the heat of ... D227/D305
Table 7. Heats of combustion of boronand beryllium derivatives.
point (OC)
Legend: 1 -. I-lame; 2 - formula; 3 density; 4 - melting
5 - boilin point (00); 6 - lower calorific value; 7 -o- kcalAg;
i 8 -.kcal/N 9 - boron; 10 - beryllium; 11 - pentaborane; 12 - de-
caborane, 13 - aluminum borohydride;.14 - beryllium borohydride;
15 - lithium borohydride; 16 - dimethyl beryllium; 17 trimethyl
boron; 18 - triethyl boron; 19 - tripropyl boron; 20 trimethyl
aluminum; 21 tetramethyl diboroethane..
Card 15/19
V
Increasing the heat of ...
Table 7.
Tablica 7-Clept o spalanta zwlqzk6w boru I berylul)
J
Nazwa
61.
Bor
13cryt Be
PIPdoborowod6r B'11.
gVzlesjqc1oborowod6r 131.111.
O)Horowodorek glinu At (1311A
O)lJormodorek berylu Be (BU.).
CsAwowocsarek -litu LfUlf,
OiDwumctyloberyi Be (CHA
CRT/rralmetylobor 13 (Cit.).
(f- Tr6jetylobor
P
B (C.14%
Qj'frr6jpropylobor D AM).
(Rerr6imetyloglin A] (Cl 1.),
gCxterometylodwubora- C
1 1. CH.
etan, ,
/D \
CH.
C11,
Card-16/19
p"A" Tern
p 0.,
to
Te, (P mina wartole-opalowa
p
C
-C
(5) kCaljkG
1 0, kcalti
2,3
l
Btu y 13670 31400'
1,01 Ma
,y 15000 2100
0,61 -m-45,% Be 15340 9630
0.92 99 - 15310 14tol
0,356. '-65,4 44.5 1=0 17670
31 $1.3 16100 -
0.666 273 roiklade siq 14300 9500.
- Staly 17700
(11900)
0.42 -20 11900
0,59
to-" 11200
0.72
-
ISO -
""0
0,73 15 125 10550
11500
2o437
P/014/61/040/005/001/002
D227/D305
20437
P/014/~1/040/005/001/002
increasing the heat of ... D227/D305
Pig. 2., Relationship between the
calorific value and the,Iratio.
(D
Legend: 1 - Upper
calorific tyfLOPAROWK
value (kcalAg); 2 -.2 ratio; I I IN MMO &I
papuNry
I'. P-11
H ,
3 - aromatics; 4 - alicyclics;
5 - alkanes; 6 - petroleum pro-
-A ducts.
5 to it f2 t3 9 Is
J 7 0
Fig. 2. ST04UNIM C:t4
20437
P/014/61/040/005/001/002
Increasing the heat of ... D227/D305
Fig. 3. Dependence of the
cal,orific.value on boiling
point.
Ito
legend: 1 Lower calorific
value (kcalAg); 2 - boiling
point, 00; 3 - alkanes; 4
alicyclics; 5 - aromatics;
6 - double-ring hydrocarbons
-bstractor's note: Not clear
ZA
whether aromatic or alicyclig.
loom
Fig. 3.
1
Card 18/19
Do WC610WOOORY PAROINOWr
_OX
8
X
1647 OW 149 WO jzU ZDU
0 TEMPIRA TURA WRIENIA, *C
Increasing the heat, of
Fig. 4. Fuel indices of various
substances.
legend: 1 - Beryllium; 2 - bo-
ron; 3 pentaborane; 4 - alu-
minum; 5 - carbon; 6 - diborane;
.7 - silicon; 6 - titanium;
9 - paraffin oil (kerosene);.
10 - acetylene; 11 - lithium
hydride; 12 - gasolene;
13 - magnesium; 14 lithium;
15 - fuel index.
P/01 ygol')J40/005/001/002
D227 "305
0, 1
UYNAIN IMAUXURKWUNY
(OwsA
nys. 4. Wspd1citynniki charaktoryA me OIA neragu substancjl
w
Fig. 4.
Card 19/1Q
266:13 P/008/61/ooo/oo8/002/003
/A 0/00 D235/D302
AUTHOR: Wislicki, Bogdan, Master of Engineering
TITLE: Dependence of the completeness of,combustion of
turbine and jet engine fuels of chemical consti-
tution
PERIODICAL: Technika lotnicza, no. 8, 1961, 171 - 178
TEXT: The effects of chemical constitution of hydrocarbon fuels
on the combustion efficiency and tendency towards coking were
investigated. Chemical characteristics of jet and turbine fuels
are specially important when they affect the physical properties.
Heat evolved in combustion is lower than the theoretical amount,
since a certain amount is wasted in side reactions such as pyro-
lysis or the formation of carbon (coking and smoking). Thermal
efficiency, , is defined as the ratio of the heat actually
obtained tor6e lower calorific value of the fuel. Complete-
ness of combustion is given byO, (=~z x 100), and may reach
Card 115
Dependence of the... 26613
P/008/61/000/008/002/003
D235/D302
94 _ 98% although 75 - 80% is more usual. The combustion process
is based fundamentally on turbulent mixing and molecular dif-
fusion of air and fuel vapor. Stability of the flame and the
rate of combustibn strongly affect Z; Thus rapid oxidation at
18oo - 20000C with a nearly thporetical amount of air should
yield continuous combustion. The mixing process at these tem-
peratures is considerably slower than the rate of combustion.
Combustion of cyclohexane in -varying amounts of air is quoted
as an illustration. Oxidation of hydrocarbons proceeds by a
chain mechanism, w-ithout branching, and is accelerated by the
products of pyrolysis, of which hydrogen is especially important
owing to its rapid ditfusion. Effects of the structural char-
acteristics of the fuel are discussed. Fuels of higher molec-
ular weight are less efficient due to their tendency towards
cracking. Self-ignition is more likely in the case of paraffins
than with aromatics and ignition is, therefore, more delayed in
the case of the latter. Pre-ignition processes have not been
fully investigated, but unfavorable re.actions at that stage may
Card 2/5
26613 P/008/61/000/008/002/003
Dependence of the... D235/D302
lower the thermal efficiency. Laboratory measurements of 0 have
been carried out, under high altitude conditions, for aviation
spirit (boiling range 53 - 1740c). Effects of the air/fuel ratios
on 0 have been investigated for kerosene, paraffin concentrate
6f'boiling range 159 - 2650C and a mixture of aromatic (75.2%)
cyclopaSaffins (11.4%) and paraffins (13.4%) boiling between 1~6
and 253 C. Values are given to show that the optimum air/fuel
ratio is -, 60, corresponding to a 0 of 98% for all the fuels
considered. The aromatic fuels became considerably less effic-
ient with high proportions of air. Design of the combustion
chamber in relation to 0 is briefly mentioned, quoting Western
sources, and experimental values of 0 are given for hydrocarbons
fed into the experimental chamber by injection or evaporation.
The effects of the chemical nature of the fuel on 0 appears to
be more Pronounced-in the latter case, 0 decreasing in the order:
paraffins > single ring cycloparaffins >cyclo-olefins > double
ring cycloparaffins > single ring aromatics with a side-chain
single ring aromatics ~> double ring aromatics. Proportions of
Card 3/5
26613 P/008/61/000/008/002/003
Dependence of the.-.-. D235/D302
the constituents and the boiling range also have an effect. In-
complete combustion results in smoking and deposition of coke or
in the elimination of soot and carbon particles in the exhaust
gases. They physical nature of smoke is briefly described,
showing that smoke is easily eliminated before coagulation into
soot. Dehydrogenation of the fuel and polymerization of the
carbon skeletons leads to coking. The effects of coke deposition
on various parts of the engine are shortly described. Coking
tendency is ultimately related to the design of the combustion
chamber, degree of atomization, surface tension, viscosity and
composition of the fuel and the amount and pressure of air.
Coking increases with increased fuel density, b.p., and in the
order: paraffins 4, cyclo-olefins < aromatics. These relation-
ships areillustrated. Within each group, coking increases with
decreased yolatility and in general increases for the higher
C ratios. Smoke formatfon increases in the series n-paraffins<
Yf iso-paraffins /_ cycloparaffins < olefins /-, cyclo-olefins <
Card 4/ 5'
26613 P/008/61/000/008/002/003
Dependence of the..... D235/D302,
di-olefin alkynes ~ n-alkyl benzenes. This is discussed andil-
lustrated. Sulphur Tompounds increase coking, but not as mucy
as the aromatics, which however do not exceed 25% in the usual
fuels. The tendency towards the inclusion of a hi5her percent-
age of less volatile components into the American P5 and JP6
fuels is mentioned. Improvement of combustion efficiency may
partially alleviate this, problem, especially during the pre-
ighition and i nitioj3 stages. W6stern work in this field is
shortly descrited.' It is believed that suitable kerosene ~~els
githout any adeitives can be PrQduced. There are 19 figures
tables and 2 references: 5 Soviet-bloc and 19 non-Soviel-
.bloc. The references to the four-most recent English-language
publications read as follows:' J Sharp, J. Royal Aeronautical
Ljoc. 58 no 528, 813~ (1954)- V:F. Massa-and B.B. Russel U.S.
Pat. 23~19,.10491, March 20 195L E.C. Aughes and 0. Hook Petr6l
71 107 (
Eng., no .19~6); and I.B. Hinkamp and V. H1nzd
Ind. Eng. Chem., 47, no. 8, 1560.~(1955)-
Card 515
WISLICKIP Bogdan, mgr.
C,
. I Combustion accuracy of fuel for turbine and rar--Jet
engines and its chemical composition. Techn lotn 16
no.8;171-178 Ag 161.
7 1
ACCESSION NR: AP3008291 P/0008/63/000/009/0233/0242
AUTHOR' Wislicki, Bogdan
TITLE: Some pro~lem;`~`offtl kinetics of chemical. processei in the combustion
chambers ofaircraft turbine engines
SOURCE: Technika lotniczal n6. 9, 1963, 233-242
TOPIC TAGS: kineticaq aircraft turbine combustion chamber- heat transfer,.
aerodynamicshydrodynimic; ignition, mass transfer
The-author defines his pa'er as "a g6neral introduction to'the kinetics
ABSTRACT: p ''I er
of th~ processes of the combustion of hydrocarb6n P und the combustion conditions
In turbine engines," remarking that there has thu's far been in Poland no
exhaustive study of this subject from the viewpoint of 'thi'kinetics of chemical
reactions at high speeds and around,2000C. Sinclelthe tate~of*combustlon and its
Intensification are.limited by the processes ofq~ heat and transfer, only a
pg its kineti
..,.total conception of the problem. gained by obsery'i' cs,-ae~rodynamics
and hydrodynamics can explain a number of phenomena and establish their regularity.
Card 1/2
ACCESSION NR: AP3008291
There are sections entitled: "Chemical kinetics of combustion reactions'
I'Mechanism of chaiii~self-lgnltlonil! "Machani*sm thermal self-ignition,11 and
"Kinetics of chemical reactions in the f I ame. 11 Original aPticle has !19 figures
and 44 numbered formulas.
ASSOCIATION: SITK, Warsaw
SUBMITTED:. 00 DATE ACQ: 1406t'63 E~
i ICL -00
SUB CODE: AC, NO REFISOV:, .00711 OTHER: 001
1z
Big
Card 2/2,
T
MIELVIKOWA, Boleslawa, doc. inz.; WISLICKI,
Bogdan, mgr.1 KLFINp64aniBJ
mgr*
Evaluation of fuels for turbojet engines. Inst lotn prace no.18t
19-33 163.
31
WISLICKI, Bogdan, mgr
Combustion procemses of hydrocartxmi fupls in fli;-I'd firjw
ongIncs. Techn lotn 19 no.6.14~-149 Je 164.
Specific heat valu-s of certaln hydrocprty)n fuelti. lbl.d.~~2
of cover, 3-4 of cover
atjTfd 4 W Pr-4
VOTMrNB, _401,TO,97 'Ap P72532/64~~W/023/00~2!003~,
I~M- ORt Wisli ki B. (Vislitskiy, 3,) (Master of arts); K
jKzUzhanovskUy., R.7~v taster engineerl
1TITLEi Mini for fuel testing
SOURCEt Warsav. Instytut Lotnictwa. Prace, no. 23, 1964, 22-35
',TOPIC TAGSt combustion chamber, fuel test, continuous combustion, vibration combus-,
!tion
ABSTRACT: J, Wolfa rf thz! Polish n1S2+ji+,j!Le has designed a small-size 1-an-
bustion cham ft,-Ft n a fuel conbustioiA investigation in order to Oefine
as
the chaxacteristics -f combustion =ih ev~aporWlon under conditions compar-nWe
to -real engine operatIng conditions. The chamber, designed for visual observa-__-)n
.of the combustion process, has been used for comparative study of B-70 gasoline and
P-2 fuel at fuel fl-w rates from 0.2 to 1.5 kg/hr. The chamber's thermal efficiency
as a function of air "xoess for the above fuels was determined. The testB conducted
have demonstruted tiir~ usefulness of microchambers for the investigation of fuel -7cm-
bustion with evaporatkon.. It has also been shown that by the use of diffusion i-f*
_k/2
L
C
.~.FA
PDrs it is Possible to intensify the vib-ati le-
fue.1 ya onal combustion-. A detailel
scriptiOn of the combustion chamber and test stand is presented, Orig. art. has: )j
formulas and 24 figu-res.
[AC]
ASSOCIATIONt Instytut Latnietwa, Warsaw (Aeronautici3 Institute)-ly
SUBMITED r COMp-r64 KIM: CID SLM CODE. F-p
REF SOV, 007- ATD PRzss.- 3220
OTHER.
9
0--)(_1)2b-67 F,.-,TP(t)/ETI IJP(c) JD/WB
ACC NR: - '_ * I
AT6033638 SOURCE CODE, PO/2532/GG/000/026/0042/0061
AUTHOR: I~Ijslicki, Bogdan -- Vislitskiy, B. (Master of Arts)
ORG: Institute of Aviation, -Warsaw (Instytut Lotnietwa)
TITLE: High efficiency laboratory fractionating column
SOURCE: Warsaw. InstyAut Lotnictwa. Prace, no. 26, 1966, 42-61
TOPIC TAGS: fractional distillation, petroleum fuel, fuel oil, resistance
thcri-nometer, petroleum refining, laboratory fractionating column, petroleum
fraction, electronic dephlegmation timer, temperature control/MET-42
temperature control unit
A13STRACT: The author discusses an automatic, laboratory- type, packed
fractionating column for distilling petroleum fuel oils and petroleum fractions unde
normal or reduced pressure, which he had designed, built, and tested. Maximum
column efficiency is about 140 theoretical plates with 1. 7-cm plate equivalent
spacing, retardation is 0. 71 milliliter liquid per plate, and a pressure drop of
0. 142 mn-i 1-1.0 per plate. The column can also be used on pilot plant scale for
fractional distillation of liquids which do not corrode the packing material. Senior
_A~
C.,d 1 2 UDC: 66.048:665.52
L 09026-6?
AT6033638
Technician Zdzislaw Kaminski of the Fuels Laboratory, Institute of Aviation,
Warsaw cncllaborate~) in constructing the column. The "L" packing material was
chosen, and the electronic timer for automatic dephlegmation control was planned
and built by Dr. A. Maczynski. Institute of Physj~;al C4~jMjqtEy,_?A1 A~ay~saw.
The 'MET-42 differential temperature control unit and the precision resistance
thermom eter, wf;,-re built at Departm ant C of Physics, Warsaw Poj)~echniSL Institute
accordincy to the design by J. Czernik, Master of Engineering. The paper was
approved by Dr. Andrzej Maczynski, Master of Arts. Orig. art. has: 32 figures,
12 tables, and 8 formulas. [Based on-author's abstract]
SU13 CODE: 11, 21/ SUBM DATE: 00Jun65j ORIG REF: 003/ SOV REF: 006/
OTH REF: 006/
ABGAR(YdICZ, Franciszek, prof. dr; BURZYNSKI, Bohdan; WISLINSKA, Irena;
WITCZAK, Franciszek
Fattening of young cattle using aDMOniated dry sugar-beet pulp
with a differing content of nitrogen compounds in the rations.
Zesz probI post nauk roln no.41:101-106 163.
.-I. Katedra Zywienia Zwierzat, Szkola Glowna Gospodarstwa
Wiejskiego, Warszawa. Kierownik: prof. F. Abgarowicz.
WISLINSKI, M.; STUDZINSKI, T.
Hematological studies on types of hemoglobin in sheeD. Acta
physiol.polon. ll,no-5/6:916-917 160.
1. Z Katedry Fisjololgii Zwierxat Wydzialu Weterynaryjnego W.S.R.
v Lublinie. Kierovnik: prof.dr. W.Holobut.
(HEMOGLaBIN)
POLAR/Chemical Technology. Chemical Products and T~heir
Application Synthetic Polymers. Plastics
Abs Jour: Ref Zhur-Khim., No 13, 1958, 45111.
Author Wisliski Tadeusz.
Inst
Title Bonding of Non-Metals. Part 11. Technology of Bonding.
Part III. Bonding Flaws and Pundamentals of Bonding
Control.
Orig Pub: Techn. lotnicza, 1956, 11, No 4, 1o6-116; No 6,
167-173-
Abstract: H. A review. The technology of preparation of ad-
hesives and of their application to non-metallic
surfaces are considered. Detailed description of
clamping procedures, heating during bond formation,
and methods for shortening the periocl of setting.
Card V2
POLAND/Chemical Technology. Chemical Products and Their
Application. Synthetic Polymers. Plastics
Abs Jour: Ref Zhur-Khim , No 13, 1958, 45111
III. Consideration of flaws arising at the surfaces
being bonded, and of their causes; fundamentals of
quality control of bonded articles and of determina-
tion of the characteristics of adhesives.
Card 2/2
H
51
I-JISLICFT, T.
Metal gluing. Pt. 2. (To be contd.)
P. 146 (Technika,Lotnicza. Vol. 12, no. 5, Sept./Oct. 1957. Warszawa, Poland)
Monthly Index of East Liirope~n Accessions (ER.Al) LC. Vol. 7, no. 2,
February 1958