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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

CARACTERISTIQUES AERODYNAMIQUES DES AILES DELTA POUR DES VITESSES DE VOL SUBSONIQUEVORONIN VI; SHVETS AI.1981; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1981; NO 6; PP. 104-109; BIBL. 10 REF.Article

EXPERIMENTALLY DETERMINED STABILITY PARAMETERS OF A SUBSONIC CASCADE OSCILLATING NEAR STALL.CARTA FO; HILAIRE AOS.1978; J. ENGNG POWER; U.S.A.; DA. 1978; VOL. 100; NO 1; PP. 111-120; BIBL. 8 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

A barely implicit correction for flux-corrected transportPATNAIK, G; GUIRGUIS, R. H; BORIS, J. P et al.Journal of computational physics (Print). 1987, Vol 71, Num 1, pp 1-20, issn 0021-9991Article

Aerodynamic design of three-dimensional subsonic wind tunnel inletsBATILL, S. M; HOFFMAN, J. J.AIAA journal. 1986, Vol 24, Num 2, pp 268-269, issn 0001-1452Article

Multiple pure tone generation in aeroengine fans at subsonic and supersonic relative tip speedsVAIDYA, P. G.AIAA journal. 1984, Vol 22, Num 10, pp 1366-1374, 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

Unsteady aspects of a low Mach number jetLAUFER, J; JIA XIANG ZHANG.The Physics of fluids. 1983, Vol 26, Num 7, pp 1740-1750, issn 0031-9171Article

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