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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

SUBSONIC AXISYMMETRIC NEAR-WAKE STUDIESMERZ RA; PAGE RH; PRZIREMBEL CEG et al.1978; A.I.A.A.J., NEW YORK; USA; DA. 1978; VOL. 16; NO 7; PP. 656-662; BIBL. 25 REF.Article

LOW-FREQUENCY APPROXIMATIONS IN UNSTEADY SMALL PERTURBATION SUBSONIC FLOWS.AMIET RK.1976; J. FLUID MECH.; G.B.; DA. 1976; VOL. 75; NO 3; PP. 545-552; BIBL. 16 REF.Article

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

RESEARCH PROGRAMME AND MEASUREMENT TECHNIQUES IN THE WATER TOWING TANK OF DFVLR IN GOETTINGENBIPPES H; MAIER A.1981; ICIASF '81. INTERNATIONAL CONGRESS ON INSTRUMENTATION IN AEROSPACE SIMULATION FACILITIES/1981/DAYTON OH; USA; NEW YORK: THE INSTITUTE OF ELECTRICAL AND ELECTRONICS ENGINEERS; DA. 1981; PP. 53-60; BIBL. 8 REF.Conference Paper

SUBSONIC/TRANSONIC CONFIGURATION AERODYNAMICSKORNER HORST.1981; ; FRA; NEUILLY-SUR-SEINE: AGARD; DA. 1981; AGARD-AR/146; 14 P.; 30 CM; BIBL. 29 REF.; ISBN 92-835-1380-0Report

EFFECT OF INTERBLADE PHASE ANGLE AND INCIDENCE ANGLE ON CASCADE PITCHING STABILITYCARTA FO; ST HILAIRE AO.1980; J. ENGNG POWER; USA; DA. 1980; VOL. 102; NO 2; PP. 391-396; BIBL. 15 REF.Article

RECENT STUDIES OF SUBSONIC VORTEX LIFT INCLUDING PARAMETERS AFFECTING STABLE LEADING-EDGE VORTEX FLOW.LAMAR JE.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 12; PP. 1205-1211; BIBL. 18 REF.Article

A NOTE ON ADAPTIVE-WALL WIND TUNNELS.SEARS WR.1977; Z. ANGEW. MATH. PHYS.; SCHWEIZ; DA. 1977; VOL. 28; NO 5; PP. 915-927; ABS. ALLEM.; BIBL. 3 REF.Article

ANALYSIS OF BLADE THICKNESS EFFECTS ON THE CASCADE OF BLADES IN SUBSONIC SHEAR FLOW.FUJITA K; NAMBA M.1977; BULL. J. S. M. E.; JAP.; DA. 1977; VOL. 20; NO 139; PP. 48-56; BIBL. 8 REF.Article

THREE-DIMENSIONAL SOLUTION OF FLOWS OVER WINGS WITH LEADING-EDGE VORTEX SEPARATION.WEBER JA; BRUNE GW; JOHNSON FT et al.1976; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 4; PP. 519-525; BIBL. 13 REF.Article

A WING-JET INTERACTION THEORY FOR USB CONFIGURATIONS.LAN CE; CAMPBELL JF.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 9; PP. 718-726; BIBL. 20 REF.Article

VERMESSUNG DES BOEENFELDES HINTER HARMONISCH SCHWINGENDEN BOEENERZEUGERN IM MODELL-UNTERSCHALL-KANAL (MUK) = MESURE DU CHAMP DE RAFALE DERRIERE DES GENERATEURS DE RAFALE A OSCILLATIONS HARMONIQUES DANS LA SOUFFLERIE SUBSONIQUE MODELEKRAG B.1982; FORSCHUNGSBERICHT- DEUTSCHE FORSCHUNGS- UND VERSUCHSANSTALT FUER LUFT- UND RAUMFAHRT; ISSN 0171-1342; DEU; DA. 1982; NO 26; 145 P.; ABS. ENG; BIBL. 16 REF.Serial Issue

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