Pascal and Francis Bibliographic Databases

Help

Search results

Your search

kw.\*:("Ecoulement hypersonique")

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 1422

  • Page / 57
Export

Selection :

  • and

AILE TRIANGULAIRE DANS UN ECOULEMENT HYPERSONIQUEGOLUBINSKIJ AI; GOLUBKIN VN.1976; DOKL. AKAD. NAUK S.S.S.R.; S.S.S.R.; DA. 1976; VOL. 226; NO 4; PP. 789-790; BIBL. 6 REF.Article

PROPULSION OPTIONS FOR THE HYPERSONIC RESEARCH AIRPLANE.VAN CAMP VV; WILLIAMS ET.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 7; PP. 611-616; BIBL. 16 REF.Article

OPTIMAL LIFT CONTROL BY MIELE'S METHOD FOR THE ATMOSPHERIC ENTRY OF A HYPERSONIC GLIDER. II. ISOPERIMETRIC TYPE PROBLEMSBEINER L.1972; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROUMAN.; DA. 1972; VOL. 17; NO 5; PP. 1039-1053; BIBL. 2 REF.Serial Issue

CALCUL DE L'ECOULEMENT HYPERSONIQUE AUTOUR D'UN CORPS A CASSURE DE LA GENERATRICE EN TENANT COMPTE DU TRANSPORT BIDIMENSIONNEL DU RAYONNEMENTZNAMENSKIJ VV.1976; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1976; NO 2; PP. 114-121; BIBL. 9 REF.Article

MINIMISATION DE LA RESISTANCE DE CORPS EN ETOILE DANS UN ECOULEMENT HYPERSONIQUE DE GAZKRAVETS VV; NYIKOLAJEV SV.1976; DOP. AKAD. NAUK UKRAJIN. R.S.R., A; S.S.S.R.; DA. 1976; NO 1; PP. 40-43; ABS. ANGL. RUSSE; BIBL. 2 REF.Article

HIGHER ORDER SIMILARITY SOLUTIONS FOR HYPERSONIC AEROFOILS.HUI WH; HEMDAN HT.sdIN: SYMMETRY, SIMILARITY GROUP THEOR. METHODS MECH. PROC. SYMP.; CALGARY; 1974; S.L.; DA. S.D.; PP. 403-417; BIBL. 7 REF.Conference Paper

LOI DES SECTIONS TRANSVERSALES POUR UNE COUCHE LIMITE TRIDIMENSIONNELLE SUR UNE AILE MINCE DANS UN ECOULEMENT HYPERSONIQUEDUDIN GN; NEJLAND V YA.1976; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1976; NO 2; PP. 75-84; BIBL. 6 REF.Article

Pressure fluctuations on hypersonic vehicles due to boundary-layer instabilitiesDEMETRIADES, A.AIAA journal. 1986, Vol 24, Num 1, pp 188-190, issn 0001-1452Article

Refinement of an alternate method for measuring heating rates in hypersonic wind tunnelsMILLER, C. G.AIAA journal. 1985, Vol 23, Num 5, pp 810-812, issn 0001-1452Article

Description analytique d'un jet gazeux hypersonique s'écoulant dans un milieu au repos ou dans un écoulement supersonique parallèleGILINSKIJ, M. M; ZAK, L. I.Izvestiâ Akademii nauk SSSR. Mehanika židkosti i gaza. 1983, Num 4, pp 183-186, issn 0568-5281Article

High speed flight vehicle structures: An overview : Flight vehicle structuresCLAY, Christopher L.Journal of aircraft. 2004, Vol 41, Num 5, pp 978-985, issn 0021-8669, 8 p.Article

Régime hypercritique de l'écoulement hypersonique autour d'une aile triangulaireDUDIN, G. N; LIPATOV, I. I.Prikladnaâ mehanika i tehničeskaâ fizika. 1985, Num 3, pp 100-106, issn 0869-5032Article

An overview of hypersonic aerothermodynamicsCHAPMAN, G. T.Communications in applied numerical methods. 1988, Vol 4, Num 3, pp 319-325, issn 0748-8025Article

Flugeigenschaftskriterien und Langzeit-Dynamik im Überschall- und HyperschallflugSACHS, G.Zeitschrift für Flugwissenschaften und Weltraumforschung. 1991, Vol 15, Num 4, pp 243-251, issn 0342-068XArticle

Propriétés hypersoniques de l'interaction régulière de deux ondes de chocTIKHOMIROV, N. A.Žurnal tehničeskoj fiziki. 1985, Vol 55, Num 1, pp 148-152, issn 0044-4642Article

Calculation of viscous hypersonic flow over a severely indented nosetipHSIEH, T.AIAA journal. 1984, Vol 22, Num 7, pp 935-941, issn 0001-1452Article

EINIGE UNTERSUCHUNGEN AN FLUGKOERPERN MIT ZENTRALSTIFT ALS STEUERORGAN BEI HOHEN MACHZAHLEN. = QUELQUES ETUDES DE MISSILES AYANT UNE POINTE COMME ORGANE DE COMMANDE AUX MEMBRES DE MACH ELEVESWYBORNY W.1977; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1977; VOL. 77; NO 3; PP. 1-30; ABS. ANGL.; BIBL. 7 REF.Serial Issue

CALCULATED HEATING ON THE AFTERBODY NOZZLE OF A HYPERSONIC AIRCRAFT CONCEPT.TALCOTT NA JR; HUNT JL.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 12; PP. 1247-1248; BIBL. 7 REF.Article

FLOW REGIMES OVER DELTA WINGS AT SUPERSONIC AND HYPERSONIC SPEEDS.SQUIRE LC.1976; AERONAUT. QUART.; G.B.; DA. 1976; VOL. 27; NO 1; PP. 1-14; BIBL. 16 REF.Article

HEATING AUGMENTATION IN EROSIVE HYPERSONIC ENVIRONMENTS.DUNBAR LE; COURTNEY JF; MCMILLEN LD et al.1975; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 7; PP. 908-912; BIBL. 10 REF.Article

HOLOGRAPHIC ANALYSIS OF PARTICLE-INDUCED HYPERSONIC BOW-SHOCK DISTORSIONS.HOVE DT; SMITH AA.1975; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 7; PP. 947-949; BIBL. 5 REF.Article

INFLUENCE DE L'ACCELERATION D'UN COIN SUR LA POSITION DU CENTRE DE PRESSION A DES VITESSES HYPERSONIQUESMEN'SHIKOVA VL; POLYANSKIJ O YU.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 6; PP. 167-170; BIBL. 4 REF.Article

A CORRELATION BETWEEN PRESSURE AND HEAT TRANSFER DISTRIBUTIONS AT SUPERSONIC AND HYPERSONIC SPEEDS.STOLLERY JL; COLEMAN GT.1975; AERONAUT. QUART.; G.B.; DA. 1975; VOL. 26; NO 4; PP. 304-312Article

CROSS-HATCHING STUDIES. A CRITICAL REVIEW.SWIGART RJ.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 10; PP. 1301-1318; BIBL. 46 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

  • Page / 57