kw.\*:("Subsonic flow")
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Comment on «A new solution method for lifting surfaces in subsonic flow»RODDEN, W. P.AIAA journal. 1984, Vol 22, Num 1, issn 0001-1452, 160Article
Clarification of turn performance of aircraftFORD, W. F.SIAM review (Print). 1996, Vol 38, Num 2, pp 309-312, issn 0036-1445Article
SUBSONIC AERODYNAMICSDELAURIER JD; REID LD.1978; INST. AEROSPACE STUD., UNIV. TORONTO, ANNU. PROGR. REP.; CAN; DA. 1978; PP. 57-58; BIBL. 7 REF.Article
THE GERMAN-DUTCH LOW SPEED WIND TUNNEL DNW.SEIDEL M; JAARSMA F.1978; AERONAUT. J.; G.B.; DA. 1978; VOL. 82; NO 808; PP. 167-173Article
QUADRATURE FORMULAS FOR CHORDWISE INTEGRALS OF LIFTING SURFACE THEORIESANDO S; ICHIKAWA A.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 3; PP. 466-467; BIBL. 6 REF.Article
ECOULEMENT NON-STATIONNAIRE D'UN GAZ DANS LE VIDE A TRAVERS UNE BARRIERE PERFOREEMILLER LG.1983; PMTF. ZURNAL PRIKLADNOJ MEHANIKI I TEHNICESKOJ FIZIKI; ISSN 0044-4626; SUN; DA. 1983; NO 2; PP. 62-65; BIBL. 3 REF.Article
HIGH-FREQUENCY SUBSONIC FLOW PAST A PULSATING THIN AIRFOIL.PLOTKIN A.1978; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1978; VOL. 16; NO 4; PP. 405-407; BIBL. 8 REF.Article
The stream structure of the solar supercoronaLOTOVA, N. A; VLADIMIRSKII, K. V; KORELOV, O. A et al.Radiophysics and quantum electronics. 1995, Vol 38, Num 9, pp 598-601, issn 0033-8443Article
Efficacité de la propulsion des corps vibrant dans un écoulement gazeux subsoniqueKOGAN, M. N; USTINOV, M. V.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1984, Num 4, pp 128-132, issn 0568-5281Article
Noniterative cross-flow integration for the pressure-split analysis of subsonic mixing-layer problemsDASH, S. M; SINHA, N.AIAA journal. 1985, Vol 23, Num 1, pp 153-155, issn 0001-1452Article
Treatment of supersonic flows with embedded subsonic regionsSHANKAR, V; SZEMA, K-Y; OSHER, S et al.AIAA journal. 1985, Vol 23, Num 1, pp 41-48, issn 0001-1452Conference Paper
Thrust augmenting ejectors. IIALPERIN, M; JIUNN-JENQ WU.AIAA journal. 1983, Vol 21, Num 12, pp 1698-1706, issn 0001-1452Article
Extension of the Blasius force theorem to subsonic speedsBARSONY-NAGY, A.AIAA journal. 1985, Vol 23, Num 11, pp 1811-1812, issn 0001-1452Article
Laminarisation de la couche limite sur une surface thermiquement isolée avec injection d'énergie dans l'écoulementKAZAKOV, A. V; KUPAREV, V. A.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1988, Num 5, pp 58-61, issn 0568-5281Article
Jet noise modification by the whistler nozzleHASAN, M. A. Z; ISLAM, O; HUSSAIN, A. K. M. F et al.AIAA journal. 1984, Vol 22, Num 3, pp 340-347, issn 0001-1452Article
AERODYNAMIQUE DES VITESSES HYPOSONIQUES (ECOULEMENTS A PETITS NOMBRES DE MACH)ZEJTUNYAN R KH.1983; PMTF. ZURNAL PRIKLADNOJ MEHANIKI I TEHNICESKOJ FIZIKI; ISSN 0044-4626; SUN; DA. 1983; NO 2; PP. 53-61; BIBL. 27 REF.Article
DOUBLET LATTICE METHOD-SCHEMES FOR CPU TIME REDUCTIONSIMHA PRASAD DS; HOLLA VS.1980; COMPUTER METHODS APPL. MECH. ENGNG; NLD; DA. 1980; VOL. 23; NO 1; PP. 59-65; BIBL. 4 REF.Article
A ONE-DIMENSIONAL ANALYSIS AND PERFORMANCE PREDICTION OF SUBSONIC RADIAL TURBINESHAMAJIMA M.1980; BULL. JSME; ISSN 0021-3764; JPN; DA. 1980; VOL. 23; NO 186; PP. 2064-2070; BIBL. 14 REF.Article
LIFTING SURFACE THEORY FOR SKEWED AND SWEPT SUBSONIC WINGSFRINK NT.1979; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS. ANNUAL MEETING AND TECHNICAL DISPLAY. 15/1979/WASHINGTON DC; USA; NEW YORK: AIAA; DA. 1979; VOL. 551; PP. 1-10; BIBL. 11 REF.Conference Paper
COMPUTER MODEL OF A FULLY DEPLOYED PARACHUTE.TORY C; AYRES R.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 7; PP. 675-679; BIBL. 5 REF.Article
REYNOLDS NUMBER EFFECTS ON BOATTAIL DRAG OF WING-BODIES.REUBUSH DE.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 5; PP. 455-459; BIBL. 18 REF.Article
SUR LE CALCUL DES ECOULEMENTS SUBSONIQUES D'UN GAZ VISQUEUX DANS L'APPROXIMATION DES EQUATIONS GENERALISEES DE PRANDTLPROKHUR NZ.1977; DINAM. SPLOSHN. SREDY; S.S.S.R.; DA. 1977; VOL. 30; PP. 112-121; BIBL. 4 REF.Article
A NOVEL CONCEPT FOR SUBSONIC INLET BOUNDARY-LAYER CONTROL.MILLER BA.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 4; PP. 403-404; BIBL. 6 REF.Article
SUMMARY OF SOME RECENT STUDIES OF SUBSONIC VORTEX LIFT AND PARAMETERS AFFECTING THE LEADING-EDGE VORTEX STABILITY.LAMAR JE.1976; IN: FLUID PLASMA DYN. CONF. 9; SAN DIEGO, CALIF.; 1976; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; VOL. 414; PP. 1-12; BIBL. 16 REF.Conference Paper
Subsonic ejector nozzle limiting flow conditionsDE CHANT, L. J.Journal of engineering for gas turbines and power. 2003, Vol 125, Num 3, pp 851-854, issn 0742-4795, 4 p.Article