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MIXING OF A TRANSVERSE JET WITH A HIGH MACH NUMBER STREAMROSEN R; HARVEY DW.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-27; 5 P.; BIBL. 9 REF.Conference Paper

DESIGN AND TEST OF TRANSONIC AIRFOILS UNDER CONSIDERATION OF DRAG DIVERGENCE MACH NUMBERKAMIYA N; NISHI T; ITOH T et al.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS FLUID AND PLASMA DYNAMICS CONFERENCE/1978/SEATTLE WA; USA; NEW YORK: AIAA; DA. 1978; 10 P.; BIBL. 6 REF.Conference Paper

RESPONSE OF A CYLINDRICAL SHELL IN SUPERSONIC FLOW TO A SHOCK LOAD.DZYGADLO Z; NOWOTARSKI I; OLEJNIK A et al.1976; J. TECH. PHYS.; POLAND; DA. 1976; VOL. 17; NO 3; PP. 279-293; ABS. POL. RUSSE; BIBL. 9 REF.Article

ETUDE EXPERIMENTALE DES JETS CIRCULAIRES SONIQUES ET SUPERSONIQUESKOVAL MA; SHVETS AI.1979; P.M.T.F.; SUN; DA. 1979; NO 4; PP. 83-89; BIBL. 4 REF.Article

AN EXTENSION OF THE MOTT-SMITH METHOD FOR SHOCK WAVESBAQUERO R.1978; BOL. INST. TONANTZINTLA; MEX; DA. 1978; VOL. 2; NO 4; PP. 327-334; ABS. SPA; BIBL. 11 REF.Article

STATISTICAL ANALYSIS OF THE VIBRATION RESPONSE OF EXTERNAL AIRCRAFT STORES.HADAN G; ESHEL R.1976; ISRAEL J. TECHNOL.; ISRAEL; DA. 1976; VOL. 14; NO 1-2; PP. 86-93; BIBL. 7 REF.; (ISR. ANNU. CONF. AVIAT. ASTRONAUT. 18. PROC.; TEL AVIV-HAIFA; 1976)Conference Paper

SPHERE DRAG AT MACH NUMBERS FROM 0.3 TO 2.0 AT REYNOLDS NUMBERS APPROACHING 107MILLER DG; BAILEY AB.1979; J. FLUID MECH.; GBR; DA. 1979; VOL. 93; NO 3; PP. 449-464; H.T. 1; BIBL. 19 REF.Article

SPEZIELLE ERWEITERUNG DER "ALLGEMEINEN FLUGZUSTANDSGLEICHUNG" = DEVELOPPEMENT SPECIAL DE L'EQUATION CARACTERISTIQUE DE VOLKLOSTER M.1979; Z. FLUGWISSENSCH. WELTR.-FORSCH.; DEU; DA. 1979; VOL. 3; NO 2; PP. 125-129; ABS. ENG; BIBL. 3 REF.Article

PERTURBATION CALCULATIONS FOR THE SPIN-UP PROBLEM USING REDUCECOHEN I; BARK F.1978; COMPUTER PHYS. COMMUNIC.; NLD; DA. 1978; VOL. 14; NO 5-6; PP. 319-326; BIBL. 8 REF.Article

ECOULEMENT AUTOUR DES CONES EMOUSSES ET DE CORPS EN FORME DE CALOTTE SPHERIQUEKARYAGIN VP; LOSHAKOV AB; SHVETS AI et al.1978; P.M.T.F.; SUN; DA. 1978; NO 5; PP. 98-102; BIBL. 6 REF.Article

THE CHARACTERISTICS OF THE PLANNED NATIONAL TRANSONIC FACILITY.MCKINNEY LW; HOWELL RR.1976; IN: AERODYN. TEST. CONF. 9. PROC.; ARLINGTON, TEX.; 1976; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; PP. 176-184; BIBL. 18 REF.Conference Paper

SUPERSONIC FLOW DEVELOPMENT IN SLOTTED WIND TUNNELSRAMASWAMY MA; CORNETTE ES.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 6; PP. 805-811; BIBL. 10 REF.Article

PERFORMANCE OF CONICAL DIFFUSERS UP TO THE CHOKING CONDITIONMARKLAND E; NORTH P.1979; CONFERENCE ON FLUID MACHINERY. 6/1979/BUDAPEST; HUN; BUDAPEST: AKAD. KIADO; DA. 1979; VOL. 2; PP. 703-714; BIBL. 7 REF.Conference Paper

DIRECTIVITY AND MACH NUMBER DEPENDENCE OF THE SOUND RADIATED FROM TURBULENT JETSCHANDRAKER AL; MUNJAL ML.1978; INDIAN J. TECHNOL.; IND; DA. 1978; VOL. 16; NO 1; PP. 18-24; BIBL. 17 REF.Article

OVERSHOOTS IN PLANETARY BOW SHOCKSRUSSELL CT; HOPPE MM; LIVESEY WA et al.1982; NATURE (LOND.); ISSN 0028-0836; GBR; DA. 1982; VOL. 296; NO 5852; PP. 45-48; BIBL. 11 REF.Article

IMPROVING THE MACH NUMBER CAPABILITIES OF ARC DRIVER SHOCK TUBESJOHNSON JA III; SANTIAGO J; LIN I et al.1980; REV. SCI. INSTRUM.; ISSN 0034-6748; USA; DA. 1980; VOL. 51; NO 10; PP. 1430-1431; BIBL. 8 REF.Article

SUR LA DEGENERESCENCE D'UN ECOULEMENT SUPERSONIQUE DANS LE CAS D'INTERACTION DES ONDES CENTREES DE COMPRESSION ET DE RAREFACTIONRYLOV AI.1979; PRIKL. MAT. MEKH.; SUN; DA. 1979; VOL. 43; NO 1; PP. 45-50; BIBL. 4 REF.Article

EFFECT OF ANGLE OF ATTACK AND MACH NUMBER ON SLENDER-WING UNSTEADY AERODYNAMICSERICSSON LE; REDING P.1978; J. AIRCR.; USA; DA. 1978; VOL. 15; NO 6; PP. 358-365; BIBL. 42 REF.Article

MACH NUMBER AND TEMPERATURE EFFECTS ON JETSLAU JC.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS FLUID AND PLASMA DYNAMIC CONFERENCE. 11/1978/SEATTLE WA; USA; NEW YORK: AIAA; DA. 1978; 78-1152; 9 P.; BIBL. 14 REF.Conference Paper

SURFACE ROUGHNESS EFFECTS ON A MACH 6 TURBULENT BOUNDARY LAYERBERG DE.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS FLUID AND PLASMA DYNAMIC CONFERENCE. 11/1978/SEATTLE WA; USA; NEW YORK: AIAA; DA. 1978; 78-1159; 8 P.; BIBL. 17 REF.Conference Paper

MACH NUMBER DEPENDENCE OF LAMINAR NEAR-WAKE TRANSITION FOR SLENDER CONES.LEGNER HH; FINSON ML.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 3; PP. 417-419; BIBL. 16 REF.Article

KINEMATIK, EINFLUSSFUNKTIONEN UND FELDGROESSEN BEI STOERUNGS-AUSBREITUNG VON BEWEGTEN STOERQUELLEN = CINEMATIQUE, FONCTIONS D'INFLUENCE ET GRANDEURS DE CHAMP POUR LA PROPAGATION DE LA PERTURBATION D'UNE SOURCE DE PERTURBATION EN MOUVEMENTARABINDO DAS.1983; FORSCHUNGSBERICHT- DEUTSCHE FORSCHUNGS- UND VERSUCHSANSTALT FUER LUFT- UND RAUMFAHRT; ISSN 0171-1342; DEU; DA. 1983; NO 1; 64 P.; ABS. ENG; BIBL. 50 REF.Serial Issue

COMPRESSIBILITY EFFECTS ON CAVITATION IN HIGH SPEED LIQUID FLOW. I: SUBSONIC LIQUID FLOWTETSUO N; OMAR FARUQUE KHAN.1981; BULL. JSME; ISSN 0021-3764; JPN; DA. 1981; VOL. 24; NO 190; PP. 648-654; BIBL. 8 REF.Article

INFLUENCE OF MACH NUMBER ON COHERENT STRUCTURE RELEVANT TO JET NOISEARMSTRONG RR JR.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 6; PP. 677-683; BIBL. 24 REF.Article

SIMULATION OF A PERPENDICULAR BOW SHOCKLEROY MM; GOODRICH CC; WINSKE D et al.1981; GEOPHYS. RES. LETT.; ISSN 0094-8276; USA; DA. 1981; VOL. 8; NO 12; PP. 1269-1272; BIBL. 17 REF.Article

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