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Results 1 to 25 of 1967

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NORMAL-FORCE AND PITCHING-MOMENT COEFFICIENTS OF WING-BODY COMBINATIONS AT VERY HIGH ANGLES OF ATTACKNIKOLITSCH D.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-63; 9 P.; BIBL. 19 REF.Conference Paper

INFLUENCE DES VARIATIONS DE L'ANGLE D'ATTAQUE SUR LE RICOCHET D'UN REDANPAVLIKEVICH BE.1977; GIDROMEKHANIKA; S.S.S.R.; DA. 1977; NO 35; PP. 35-39; BIBL. 2 REF.Article

THE FORBUSH PREDECREASEGOLD RE; PEACOCK DS.1973; J. GEOPHYS. RES.; U.S.A.; DA. 1973; VOL. 78; NO 4; PP. 577-587; BIBL. 27REF.Serial Issue

INTERNAL FLOW CALCULATIONS FOR AXISYMMETRIC SUPERSONIC INLETS AT ANGLE OF ATTACK.PRESLEY LL.1975; IN: AM. INST. AERONAUT. ASTRONAUT.-SOC. AUTOMOT. ENG. PROPUL. CONF. 11; ANAHEIM, CALIF.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1214; PP. 1-7; BIBL. 11 REF.Conference Paper

ECOULEMENT HYPERSONIQUE D'UNE AILE TRIDIMENSIONNELLEKRAVETS VV; KHRUSHCH VK.1975; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1975; VOL. 18; NO 4; PP. 94-100; BIBL. 6 REF.Article

WING-ALONE AERODYNAMIC CHARACTERISTICS AT HIGH ANGLES OF ATTACKSTALLINGS RL JR; LAMB M.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 7 P.; BIBL. 6 REF.Conference Paper

A METHOD FOR CALCULATING THE AERODYNAMIC FORCES AND MOMENTS ON EXTERNAL STORES OF AIRCRAFTRONEN T; HANIN M.1979; ISRAEL ANNUAL CONFERENCE ON AVIATION AND ASTRONAUTICS. 21/1979-02-28/TEL AVIV, HAIFA; ISR; HAIFA: AYALON OFFSET; DA. 1979; PP. 176-181; BIBL. 11 REF.Conference Paper

EFFECTS OF REYNOLDS NUMBER ON SWEPT-WING-BODY CONFIGURATIONS WITH HIGH LIFT DEVICES AT TRANSONIC SPEEDS.ATRAGHJI E; SORENSEN H.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 94-120; BIBL. 8 REF.Conference Paper

PITCH ANGLE DISTRIBUTION OF SOLAR FLARE PARTICLES IN INTERPLANETARY SPACEMAURER RH; DUGGAL SP; POMERANTZ MA et al.1973; J. GEOPHYS. RES.; U.S.A.; DA. 1973; VOL. 78; NO 1; PP. 29-36; BIBL. 20 REF.Serial Issue

ECHAPPEMENT DES PARTICULES ENERGETIQUES D'ALBEDO DE L'ATMOSPHERE VERS L'ESPACE COSMIQUEGRIGOROV NL.1982; GEOMAGN. AERON.; ISSN 0016-7940; SUN; DA. 1982; VOL. 22; NO 2; PP. 197-204; BIBL. 8 REF.Article

SEPARATION AND REATTACHMENT NEAR THE LEADING EDGE OF A THIN AIRFOIL AT INCIDENCECEBECI T; STEWARTSON K; WILLIAMS PG et al.1981; AGARD CONF. PROC.; ISSN 0549-7191; FRA; DA. 1981; NO 291; PP. 20.1-20.13; BIBL. 25 REF.Article

WIND TUNNEL CORRECTIONS FOR HIGH ANGLE OF ATTACK MODELS1981; ; FRA; NEUILLY-SUR-SEINE: AGARD; DA. 1981; AGARD/R-692; 124 P.; 30 CM; BIBL. DISSEM.; ISBN 92-835-0283-3Report

ESTIMATION OF TRANSONIC AIRCRAFT AERODYNAMICS TO HIGH ANGLES OF ATTACK.XELSON JA.1975; IN: AM. INST. AERONAUT. ASTRONAUT. AIRCR. SYST. TECHNOL. MEET.; LOS ANGELES; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 996; PP. 1-9; BIBL. 23 REF.Conference Paper

INFLUENCE DE L'ANGLE D'ATTAQUE SUR LES CARACTERISTIQUES D'UN ETAGE DE TURBINE AXIALEMAKSUTOVA MK; VAVILOV GA; TARASOV VN et al.1974; IZVEST. VYSSH. UCHEBN. ZAVED., ENERGET.; S.S.S.R.; DA. 1974; VOL. 17; NO 8; PP. 74-78; BIBL. 7 REF.Article

STRONG PITCH ANGLE DIFFUSION AND MAGNETOSPHERIC SOLAR PROTONSWILLIAMS DJ; HEURING FT.1973; J. GEOPHYS. RES.; U.S.A.; DA. 1973; VOL. 78; NO 1; PP. 37-50; BIBL. 1 P.Serial Issue

THE ANALYSIS OF WING-BODY COMBINATIONS AT MODERATE ANGLES OF ATTACKUCHIYAMA N; MIKKILINENI RP; WU JM et al.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-62; 6 P.; BIBL. 10 REF.Conference Paper

WIND-TUNNEL INVESTIGATION OF DIFFERENT MISSILE CONFIGURATIONS AT ANGLES OF ATTACK UP TO 30 DEGREES AND MACH NUMBERS 0.6 TO 3.5ENDMANN P.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-22; 7 P.; BIBL. 2 REF.Conference Paper

OSCILLATIONS HARMONIQUES D'UNE AILE ANNULAIRE DANS L'ECOULEMENT STATIONNAIRE D'UN FLUIDE PARFAITSHESTERNIA ZN.1978; IZVEST. VYSSH. UCHEBN. ZAVED., AVIATC. TEKH.; SUN; DA. 1978; VOL. 21; NO 2; PP. 115-121; BIBL. 7 REF.Article

SOME CONCLUSIONS FROM AN INVESTIGATION OF BLADE-VORTEX INTERACTION.HAM ND.1975; J. AMER. HELICOPTER SOC.; U.S.A.; DA. 1975; VOL. 20; NO 4; PP. 26-31; BIBL. 6 REF.Article

DETERMINATION DES CARACTERISTIQUES AERODYNAMIQUES D'UN CONE AVEC DE FAIBLES DEVIATIONS ARBITRAIRES DE SURFACEGOMAN OG; DAVYDOV VI.1975; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1975; VOL. 18; NO 4; PP. 58-62; BIBL. 1 REF.Article

AERODYNAMIC CHARACTERISTICS OF AN AXISYMMETRIC BODY UNDERGOING A UNIFORM PITCHING MOTION.SMITH LH; NUNN RH.1975; IN: ANN. INST. AERONAUT. ASTRONAUT. 8TH FLUID PLASMA DYN. CONF.; HARTFORD, CONN.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 838; PP. 1-9; BIBL. 15 REF.Conference Paper

EFFET DE L'ANGLE D'ATTAQUE SUR LES PERTES DE CHARGE DUES AU PROFIL DANS UNE GRILLE DE TURBINE A REFROIDISSEMENT PAR TRANSPIRATIONEPIFANOV VM; GUS'KOV VI.1980; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; SUN; DA. 1980; NO 1; PP. 37-40; BIBL. 6 REF.Article

STRAKE-WING ANALYSIS AND DESIGNLAMAR JE.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS FLUID AND PLASMA DYNAMICS CONFERENCE. 11/1978/SEATTLE WA; USA; NEW YORK: AIAA; DA. 1978; 78-1201; 11 P.; BIBL. 14 REF.Conference Paper

STRUCTURES TOURBILLONNAIRES DES AILES MINCES DANS LE CAS D'ECOULEMENT DECOLLEKARASK AA; NISHT MI.1979; DOKL. AKAD. NAUK S.S.S.R.; SUN; DA. 1979; VOL. 246; NO 6; PP. 1317-1320; BIBL. 4 REF.Article

EXPERIMENTAL OBSERVATIONS OF WALL INTERFERENCE AT TRANSONIC SPEEDSSTARR RF JR.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 9 P.; BIBL. 6 REF.Conference Paper

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