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FLOW VISUALIZATION IN SUPERSONIC FLOWSRAPAGNANI NL; DAVIS SJ.1980; A.C.S. SYMP. SER.; ISSN 0097-6156; USA; DA. 1980; NO 134; PP. 167-172; BIBL. 6 REF.Article

PHASE PREPARATOIRE A L'ETUDE DE LA DECHARGE ELECTRIQUE DANS UN GAZ EN MOUVEMENTJAEGGY BC; JOECKLE R; STERN G et al.1972; ISL-20-72; DTSCH.; DA. 1972; PP. 1-19; H.T. 7; ABS. ALLEM.; BIBL. 1 P. 1/2Report

COMPARISON OF LAMP AND BLAZER CODE CALCULATIONS WITH TRW CL XV MEASUREMENTSO'KEEFE D; SUGIMURA T; BEHRENS W et al.1979; OPT. ENGNG; USA; DA. 1979; VOL. 18; NO 4; PP. 363-369; BIBL. 7 REF.Article

ACOUSTIC SUPPRESSION IN A PULSED CHEMICAL LASERAUSHERMAN DR; ALBER IE; BAUM E et al.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-237; 9 P.; BIBL. 6 REF.Conference Paper

TURBULENT FLUCTUATIONS IN THE WAKES OF GASDYNAMIC LASER CUSPS.DEMETRIADES A.1978; J. ENERGY; U.S.A.; DA. 1978; VOL. 2; NO 2; PP. 124-126; BIBL. 6 REF.Article

DEVELOPMENT AND APPLICATION OF LASER ANEMOMETRY TO TURBULENT HIGH SPEED FLOWS.ARDONCEAU P; BOUE F; LEBLANC R et al.1976; ISL-R-117-76; FR.; DA. 1976; PP. 119-165; BIBL. 11 REF.; (WORKSHOP LASER ANEMOM. PROC.; SAINT-LOUIS; 1976)Conference Paper

TWO-DIMENSIONAL SUPERSONIC DIFFUSER EXPERIMENTS.HASINGER SH; MILLER DK.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 4; PP. 536-538; BIBL. 9 REF.Article

SYSTEME D'EQUATIONS APPROCHE POUR LE CALCUL DES ECOULEMENTS TRIDIMENSIONNELS SUPERSONIQUES PAR LA METHODE DES CARACTERISTIQUESBORISOV VM.1976; DOKL. AKAD. NAUK S.S.S.R.; S.S.S.R.; DA. 1976; VOL. 228; NO 4; PP. 813-816; BIBL. 6 REF.Article

NEAR-FIELD SUPERSONIC FLOW PATTERN OF SLENDER DELTA WINGS.CHAUDHURI SN; PRAHARAJ SC.1975; INTERNATION. J. ENGNG SCI.; G.B.; DA. 1975; VOL. 13; NO 9-10; PP. 889-904; BIBL. 17 REF.Article

ECOULEMENT SUPERSONIQUE ET NON STATIONNAIRE SUR DES CORPS LORS D'UN BRUSQUE FREINAGETURCHAK LI.1976; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1976; NO 1; PP. 166-170; BIBL. 8 REF.Article

ADVANCED SUPERSONIC INLET TECHNOLOGY = TECHNOLOGIE DES ENTREES D'AIR SUPERSONIQUES DE CONCEPTION AVANCEESORENSEN NE; SMELTZER DB; LATHAM EA et al.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 5; PP. 278-282; BIBL. 13 REF.Serial Issue

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

FLOWFIELD IN THE PLANE OF SYMMETRY BELOW A DELTA WING.CRAMER MS; GEORGE AR; SEEBASS AR et al.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 2; PP. 212-215; BIBL. 2 REF.Article

ETUDE DES ECOULEMENTS SUPERSONIQUES DANS LES TUYERES CONIQUESPIRUMOV UG; ROSLYAKOV GS; SUKHORUKOV VP et al.1974; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1974; NO 3; PP. 101-107; BIBL. 6 REF.Article

ZUR SIMULATION EINES UNTEREXPANDIERTEN TREIBSTRAHLS BEI DER UNTERSUCHUNG DER STATISCHEN LAENGSSTABILITAET EINES ACHSENSYMMETRISCHEN FLUGKOERPERS IN EINER UEBERSCHALLSTROEMUNG. = SIMULATION D'UN JET PROPULSIF SOUS-DETENDU POUR L'ETUDE DE LA STABILITE STATIQUE LONGITUDINALE D'UN VEHICULE AXISYMETRIQUE EN VOL A VITESSE SUPERSONIQUE)EMUNDS H; RIEDEL H.1976; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1976; VOL. 76; NO 21; PP. 1-65; ABS. ANGL.; BIBL. 3 REF.Serial Issue

ETUDE DE L'ECOULEMENT SUPERSONIQUE AUTOUR D'UN CONE ELLIPTIQUE POINTU SOUS UN ANGLE D'ATTAQUEVETLUTSKIJ VN; GANIMEDOV VL.1975; P.M.T.F.; S.S.S.R.; DA. 1975; NO 1; PP. 114-120; BIBL. 18 REF.Article

ZUM AUFTRIEBSPROBLEM VON TRAGFLUEGELN MIT WOELBUNG UND VERWINDUNG BEI UEBERSCHALLSTROEMUNG. = PROBLEME DE PORTANCE DES AILES PORTANTES AVEC CAMBRURE ET GAUCHISSEMENT DANS DES ECOULEMENTS SUPERSONIQUESDAS A.1975; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 10; PP. 1-60; ABS. ANGL.; BIBL. 3 P.Article

GAS-DYNAMIC PHENOMENA IN CHEMICAL LASERS.SKIFSTAD JG.1974; ACTA ASTR.; G.B.; DA. 1974; VOL. 1; NO 5-6; PP. 781-812; BIBL. 4 P.; (4TH INT. COLLOQ. GASDYN. EXPLOS. REACT. SYST.; LA JOLLA, CALIF.; 1973)Conference Paper

MEASUREMENTS IN THE NEAR FIELD OF SUPERSONIC NOZZLES FOR CHEMICAL LASER SYSTEMS.WHITFIELD DL; LEWIS JWL; WILLIAMS WD et al.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 6; PP. 870-872; BIBL. 5 REF.Article

STRUCTURE OF A SUPERSONIC WET-STEAM FLOW IN STRAIGHT NOZZLES.ZYSINA MOLOZHEN LM; MITENKOV VB; SOSKOVA IN et al.1974; HEAT TRANSFER, SOVIET RES.; U.S.A.; DA. 1974; VOL. 6; NO 1; PP. 109-115; BIBL. 7 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

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