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kw.\*:("SUPERSONIC FLOW")

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Results 1 to 25 of 4749

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ETUDE EXPERIMENTALE DE L'ECOULEMENT AUTOUR D'UN COIN DE LARGEUR FINIEVINOGRADOV VA; DUGANOV VV; ZAKHAROV NN et al.1979; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; SUN; DA. 1979; NO 4; PP. 106-108; BIBL. 5 REF.Article

ETUDE THEORIQUE ET EXPERIMENTALE DES CARACTERISTIQUES AERODYNAMIQUES DE CORPS TRIDIMENSIONNELSGUSAROV AA; DVORETSKIJ VM; IVANOV M YA et al.1979; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; SUN; DA. 1979; NO 3; PP. 97-102; BIBL. 11 REF.Article

ETUDE EXPERIMENTALE DE LA RESISTANCE DES AILES AUX VITESSES SUPERSONIQUESBRODETSKIJ MD; KOSORYGIN VS; RAFAEHLYANTS AA et al.1977; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH. NAUK; S.S.S.R.; DA. 1977; NO 2; PP. 47-53; BIBL. 8 REF.Article

FORMULE DE RESISTANCE POUR LES PARTIES ANTERIEURES ALLONGEES DES APPAREILS VOLANTSFOLLEH MI.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 3; PP. 156-160; BIBL. 6 REF.Article

RESEAUX SUPERSONIQUES DES DERNIERS ETAGES DES TURBINES A VAPEUR PUISSANTESTROYANOVSKIJ BM; MAJORSKIJ EV; LUKIN VV et al.1977; TEPLOENERGETIKA; S.S.S.R.; DA. 1977; NO 10; PP. 7-12; BIBL. 18 REF.Article

A SEMIEMPIRICAL METHOD FOR PREDICTING NORMAL FORCE AND CENTRE OF PRESSURE CHARACTERISTICS OF WING BODY COMBINATIONS AT SUPERSONIC SPEEDS INCLUDING THE NONLINEAR EFFECTS OF BODY CROSSFLOW.SHANKA NARAYAN SESHADRI.1977; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1977; VOL. 77; NO 7; PP. 1-44; ABS. ALLEM.; BIBL. 1 P.Serial Issue

ICE-CRYSTAL/SHOCK-LAYER INTERACTION IN HYPERSONIC FLIGHT.LIN TC; THYSON NA.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 10; PP. 1511-1514; BIBL. 14 REF.Article

SHOCK WAVES AHEAD OF A FAN WITH NONUNIFORM BLADESCARGILL AM.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 4; PP. 572-578; BIBL. 15 REF.Article

SOME EFFECTS OF CRUISE SPEED AND ENGINE MATCHING ON SUPERSONIC INLET DESIGNBANGERT LH; SANTMAN DM; HORIE G et al.1982; J. AIRCR.; ISSN 0021-8669; USA; DA. 1982; VOL. 19; NO 1; PP. 58-64; BIBL. 8 REF.Article

A THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE CONSTANT AREA, SUPERSONIC-SUPERSONIC EJECTORDUTTON JC; MIKKELSEN CD; ADDY AL et al.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 10; PP. 1392-1400; BIBL. 12 REF.Article

GASDYNAMIC PROCESSES OF PROPOSED LASER PULSE PROPULSION DEVICESAGEEV VP; BARCHUKOV AI; BUNKIN FV et al.1981; PROG. ASTRONAUT. AERONAUT.; ISSN 0079-6050; USA; DA. 1981; VOL. 76; PP. 33-45; BIBL. 10 REF.Conference Paper

EFFET DES PROPRIETES D'UNE SOLUTION STATIONNAIRE LIMITE SUR L'ETABLISSEMENT (DE CETTE SOLUTION)BLOKHIN AM; ROMENSKIJ EI.1980; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH. NAUK; SUN; DA. 1980; NO 1; PP. 44-50; BIBL. 7 REF.Article

APPLICABILITY OF AXISYMMETRIC ANALYSIS IN PREDICTING SUPERSONIC FLOW THROUGH ANNULAR CASCADES.FRUEHAUF HH.1977; J. ENGNG POWER; U.S.A.; DA. 1977; VOL. 99; NO 1; PP. 115-120; BIBL. 5 REF.Article

SUR CERTAINES APPROCHES DES PROBLEMES SPATIAUX D'OPTIMISATION DANS L'AERODYNAMIQUUE SUPERSONIQUEDULOV VG.1976; P.M.T.F.; S.S.S.R.; DA. 1976; NO 5; PP. 69-77; BIBL. 4 REF.Article

AILES DELTA ANTISYMETRIQUES D'ORDRE SUPERIEUR EN REGIME SUPERSONIQUESTAICU S.1981; BUL. INST. POLITECH. "GHEORGHE GHEORGHIN-DEJ" BUCARESTI, MEC.; ROM; DA. 1981; VOL. 43; NO 3; PP. 11-20; ABS. RUM; BIBL. 4 REF.Article

ANALYSE DES PERFORMANCES ET LIMITES DE FONCTIONNEMENT DES EJECTEURS SUPERSONIQUES EN PRESENCE D'UNE INJECTIONROBERT C.1980; ENTROPIE; ISSN 0013-9084; FRA; DA. 1980; VOL. 16; NO 92; PP. 8-14; ABS. ENG/GER/SPA; BIBL. 21 REF.Article

STUDIU CALITATIV SI CANTITATIV AL AMORSARII CURGERII SUPERSONICE PRIN RETELE DE PALETE = ETUDE QUALITATIVE ET QUANTITATIVE D'UN ECOULEMENT SUPERSONIQUE A TRAVERS UNE CASCADE D'AUBESSTANCIU V.1980; BUL. INST. POLITEH. "GHEORGE GHEORGHIU-DEJ" BUCURESTI, MEC.; ROM; DA. 1980; VOL. 42; NO 2; PP. 81-86; ABS. ENG; BIBL. 3 REF.Article

PROBABILISTIC APPROACH TO RADIATIVE TRANSFER IN SUPERSONIC FLOWSNOERDLINGER PD.1979; ASTROPHYS. SPACE SCI.; NLD; DA. 1979; VOL. 61; NO 1; PP. 185-194; BIBL. 15 REF.Article

WELLENAUSBREITUNG AN FLUEGELN = PROPAGATION DES ONDES SUR LES AILESOSWATITSCH K.1979; Z. FLUGWISSENSCH. WELTR.-FORSCH.; DEU; DA. 1979; VOL. 3; NO 3; PP. 149-156; ABS. ENGArticle

OPTIMUM TWO DIMENSIONAL WINGS IN SUPERSONIC FLOWSDUTT HNV; SREEKAHNTH AK.1978; J. ASTRONAUT. SCI.; USA; DA. 1978; VOL. 26; NO 3; PP. 279-287; BIBL. 4 REF.Article

UNSTEADY SUPERSONIC AERODYNAMIC THEORY BY THE METHOD OF POTENTIAL GRADIENT.JONES WP; APPA K.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 1; PP. 59-65; BIBL. 23 REF.Article

AERODYNAMIQUE STATIONNAIRE LINEARISEE II (SUPERSONIQUE).HOMENTCOVSCHI D.1977; ARCH. MECH.; POLAND; DA. 1977; VOL. 29; NO 1; PP. 41-51; ABS. POL. RUSSE; BIBL. 7 REF.Article

AN EXPERIMENTAL DETERMINATION OF THE UNSTREADY AERODYNAMICS IN A CONTROLLED OSCILLATING CASCADE.FLEETER S; NOVICK AS; RIFFEL RE et al.1977; J. ENGNG POWER; U.S.A.; DA. 1977; VOL. 99; NO 1; PP. 88-96; BIBL. 9 REF.Article

APPLICATION OF THE FINITE ELEMENT TECHNIQUE COMBINED WITH THE COLLOCATION METHOD TO LOW SUPERSONIC LIFTING SURFACE PROBLEMS.HASHIMOTO M; WASHIZU K.1977; INTERNATION. J. NUMER. METHODS ENGNG; G.B.; DA. 1977; VOL. 11; NO 10; PP. 1559-1577; BIBL. 22 REF.Article

THE INDEPENDENCE OF UPPER AND LOWER WING FLOWS AT SUPERSONIC SPEEDS.SQUIRE LC.1976; AERONAUT. J.; G.B.; DA. 1976; VOL. 80; NO 790; PP. 452-456; BIBL. 4 REF.Article

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