Pascal and Francis Bibliographic Databases

Help

Search results

Your search

kw.\*:("CORPS ELANCE")

Document Type [dt]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Publication Year[py]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Discipline (document) [di]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Language

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Author Country

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Results 1 to 25 of 426

  • Page / 18
Export

Selection :

  • and

ESTIMATION OF AERODYNAMICS FOR SLENDER BODIES ALONE AND WITH LIFTING SURFACES AT ALPHA 'S FROM 0O TO 90OJORGENSEN LH.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 3; PP. 409-412; BIBL. 7 REF.Serial Issue

INTEGRALGLEICHUNGEN ZUR BERECHNUNG DER UMSTROEMUNG BESCHLEUNIGTER SCHLANKER KOERPER FUER M1. = EQUATIONS INTEGRALES POUR LE CALCUL DE L'ECOULEMENT AUTOUR DE CORPS ELANCES ACCELERES POUR M1BALLMANN J.1975; Z. ANGEW. MATH. MECH.; DTSCH.; DA. 1975; VOL. 55; NO 4; PP. 114-115; BIBL. 3 REF.; (WISS. JAHRESTAG. GES. ANGEW. MATH. MECH. VORTR.; BOCHUM; 1974)Conference Paper

COMMENT ON "APPROXIMATE CALCULATION OF VORTEX TRAJECTORIES OF SLENDER BODIES AT INCIDENCE". REPLY BY AUTHOR TO W.L. OBERKAMPFOBERKAMPF WL; WEIHS D.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 2; PP. 317-318; BIBL. 10 REF.Article

INTEGRAL APPROXIMATION FOR SLENDER-BODY SHOCK SHAPES IN HYPERSONIC FLOW.FIORINO TD; RASMUSSEN ML.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 2; PP. 1735-1737; BIBL. 8 REF.Article

NON-LINEARITE DANS LA PORTANCE DE CORPS ELANCES EN INCIDENCE. INTRODUCTION D'UN NOUVEAU MODELE DE COUCHE TOURBILLONNAIREMATSUMURA K; TANAKA I; SAKUMA S et al.1982; J. SOC. NAVAL ARCHIT. JPN.; ISSN 0514-8499; JPN; DA. 1982-07; VOL. 151; PP. 65-74; ABS. ENG; BIBL. 17 REF.Article

SIDE FORCES ON UNYAWED SLENDER INCLINED AERODYNAMIC BODIES.KAO HC.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 3; PP. 142-150; BIBL. 15 REF.Article

ON BOUNDARY VALUE PROBLEMS FOR THE DOMAIN EXTERIOR TO A THIN OR SLENDER REGIONHOMENTCOVSCHI D.1983; ZEITSCHRIFT FUER ANGEWANDTE MATHEMATIK UND PHYSIK; ISSN 0044-2275; CHE; DA. 1983; VOL. 34; NO 3; PP. 322-333; ABS. FRE; BIBL. 24 REF.Article

THE DIFFRACTION OF A SHOCK WAVE BY A SLENDER BODY.MORGAN K.1975; Z. ANGEW. MATH. PHYS.; SCHWEIZ; DA. 1975; VOL. 26; NO 1; PP. 13-29; ABS. ALLEM.; BIBL. 7 REF.Article

CLASSE DE SOLUTIONS DE SIMILITUDE DES PROBLEMES D'ECOULEMENT HYPERSONIQUE DES CORPS DE REVOLUTION POREUXANTONOV AM; ZAJTSEV AV.1974; PRIKL. MEKL., U.S.S.R.; S.S.S.R.; DA. 1974; VOL. 10; NO 12; PP. 89-94; BIBL. 8 REF.Article

SCATTERING BY SLENDER BODIES OF REVOLUTIONJUNGER MC.1982; JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA; ISSN 0001-4966; USA; DA. 1982; VOL. 72; NO 6; PP. 1954-1956; BIBL. 7 REF.Article

INFLUENCE DE LA ROTATION SUR LES CARACTERISTIQUES AERODYNAMIQUES DE CORPS AXISYMETRIQUES, DE GRAND ALLONGEMENT, A DES VITESSES SUPERSONIQUESBYCHKOV NM; ISHTULOV AG; KOVALENKO VM et al.1981; IZV. SIB. OTD. AKAD. NAUK SSSR, SER. TEH. NAUK; ISSN 0002-3434; SUN; DA. 1981; NO 3; PP. 65-74; BIBL. 11 REF.Article

MAGNETOHYDRODYNAMICAL UNSTEADY FLOW PAST A SLENDER BODY OF AN ARBITRARY CROSS-SECTION.SUWA S; KUSUKAWA K.1974; J. PHYS. SOC. JAP.; JAP.; DA. 1974; VOL. 36; NO 4; PP. 1174-1184; BIBL. 15 REF.Article

ERWEITERUNG DER PARABOLISCHEN METHODE FUER SCHALLNAHE STROEMUNGEN: INSTATIONAERE STROEMUNG. = EXTENSION DE LA METHODE PARABOLIQUE POUR DES ECOULEMENTS TRANSSONIQUES: ECOULEMENT NON STATIONNAIREOEHMEN KH; TEIPEL I.1975; Z. ANGEW. MATH. MECH.; DTSCH.; DA. 1975; VOL. 55; NO 4; PP. 145-146; BIBL. 4 REF.; (WISS. JAHRESTAG. GES. ANGEW. MATH. MECH. VORTR.; BOCHUM; 1974)Conference Paper

AXISYMMETRIC SONIC FLOW COMPUTED BY A NUMERICAL METHOD APPLIED TO SLENDER BODIES.SEDIN YCJ.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 4; PP. 504-511; BIBL. 19 REF.Article

EVALUATION OF DRAG INTEGRAL USING CUBIC SPLINES.JAMES RM; PANICO VD.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 8; PP. 494-496; BIBL. 4 REF.Article

THEORETICAL PREDICTION OF ROLL MOMENTS ON FINNED BODIES IN SUPERSONIC FLOW.OBERKAMPF WL.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 111; PP. 1-8; BIBL. 11 REF.Conference Paper

AERODYNAMIC FORCES AND MOMENTS ON A SLENDER WITH A JET PLUME FOR ANGLES OF ATTACK UP TO 180 DEGREES.FLEEMAN EL; NELSON RC.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 110; PP. 1-15; BIBL. 25 REF.Conference Paper

AXISYMMETRIC SONIC FLOW COMPUTED BY A NUMERICAL METHOD APPLIED TO SLENDER BODIES.SEDIN YCJ.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 544; PP. 1-12; BIBL. 16 REF.Conference Paper

COMPUTATIONAL STUDY OF THE MAGNUS EFFECT ON BOATTAILED SHELLSTUREK WB; MYLIN DC.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 10; PP. 1462-1464; BIBL. 5 REF.Article

SUR LA REGULARITE DE LA FONCTION DE GREEN DU PROBLEME DE NEUMANN-KELVINEUVRARD D.1982; REV. ROUM. MATH. PURES APPL.; ISSN 0035-3965; ROM; DA. 1982; VOL. 27; NO 3; PP. 319-326; BIBL. 13 REF.Article

NAVIER-STOKES SOLUTION OF A SLENDER BODY OF REVOLUTION AT LARGE INCIDENCEHANKEY WL; GRAHAM JE; SHANG JS et al.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 8 P.; BIBL. 15 REF.Conference Paper

PREDICTION OF YAWING FORCE AT HIGH ANGLE OF ATTACK.WARDLAW AB JR.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 8; PP. 1142-1144; BIBL. 9 REF.Article

DER EINFLUSS GEOMETRISCHER PARAMETER AUF DIE MESSUNG DES STATISCHEN DRUCKES IN VERDUENNTER HYPERSCHALLSTROEMUNG. = INFLUENCE DES PARAMETRES GEOMETRIQUES SUR LA MESURE DE LA PRESSION STATIQUE EN ECOULEMENT HYPERSONIQUE RAREFIEKIENAPPEL K.1974; Z. FLUGWISSENSCH.; DTSCH.; DA. 1974; VOL. 22; NO 7; PP. 240-248; ABS. ANGL. FR.; BIBL. 20 REF.Article

DIE UNTERSUCHUNG DER SCHALLNAHEN UBERSCHALLSTROEMUNG UM SCHLANKE PROFILE = ETUDE DE L'ECOULEMENT SUPERSONIQUE AU VOISINAGE DE LA VITESSE DU SON AUTOUR DE PROFILS DE FORME ELANCEEFRANK W.1973; Z. ANGEW. MATH. MECH.; DTSCH.; DA. 1973; VOL. 53; NO 4; PP. 97-99; BIBL. 2 REF.; (VORTR. WISS. JAHRESTAG. GES. ANGEW. MATH. MECH.; LJUBLJANA; 1972)Conference Paper

THE EFFECT OF ROLL ANGLE ON THE FLOW OVER A SLENDER BODY OF REVOLUTION AT HIGH ANGLES OF ATTACKDEXTER PC; HUNT BL.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 13 P.; BIBL. 18 REF.Conference Paper

  • Page / 18