MODELING PROCEDURES FOR HANDLING QUALITIES EVALUATION OF FLEXIBLE AIRCRAFTGOVINDARAJ KS; EULRICH BJ; CHALK CR et al.sdANNUAL ALLERTON CONFERENCE ON COMMUNICATION, CONTROL AND COMPUTING. 19/1981/MONTICELLO IL; USA; DA. S.D.; PP. 329-338; BIBL. 3 REF.Conference Paper

ALTITUDE TRANSITIONS IN ENERGY CLIMBWESTON AR; CLIFF EM; KELLEY HJ et al.1983; AUTOMATICA (OXFORD); ISSN 0005-1098; GBR; DA. 1983; VOL. 19; NO 2; PP. 199-202; BIBL. 16 REF.Article

AN EFFECTIVE ENVIRONMENTAL CONTROL SYSTEM FOR A SUPERSONIC AIR LAUNCHED MISSILEGONZALEZ JI.1980; INSTRUMENTATION IN THE AEROSPACE INDUSTRY. ADVANCES IN TEST MEASUREMENT. INTERNATIONAL INSTRUMENTATION SYMPOSIUM. 26/1980/SEATTLE WA; USA; RESEARCH TRIANGLE PARK NC: INSTRUMENT SOCIETY OF AMERICA; DA. 1980; VOL. 2; PP. 543-552; BIBL. 1 REF.Conference Paper

HIGH-VELOCITY FEATURES IN M42 DRIVEN BY STELLAR WINDSTAYLOR K; MUNCH G.1978; ASTR. AND ASTROPHYS.; DEU; DA. 1978; VOL. 70; NO 3; PP. 359-366; BIBL. 34 REF.Article

DISSIPATION OF SUPERSONIC TURBULENCE IN INTERSTELLAR CLOUDSSCALO JM; PUMPHREY WA.1982; ASTROPHYSICAL JOURNAL; ISSN 0004-637X; USA; DA. 1982; VOL. 258; NO 1; PART. 2; PP. L29-L33; BIBL. 29 REF.Article

NON EQUILIBRIUM RADIATION OF A SHOCK WAVE AHEAD OF A BLUNT BODYKUZ'MIN AG.1981; Z. TEH. FIZ.; ISSN 0044-4642; SUN; DA. 1981; VOL. 51; NO 1; PP. 215-217; BIBL. 4 REF.Article

ROLE DE LA COMPRESSIBILITE DANS LE PROCESSUS D'INTERACTION A GRANDE VITESSE ENTRE CORPS SOLIDESZLATIN NA; KOZHUSHKO AA.1980; FIZ. GOREN. VZRYVA; ISSN 0430-6228; SUN; DA. 1980; VOL. 16; NO 5; PP. 94-96; BIBL. 13 REF.Article

LAENGSSTABILITAET IM UEBERSCHALL- UND HYPERSCHALLFLUG. = STABILITE LONGITUDINALE EN VOL SUPERSONIQUE ET HYPERSONIQUESACHS G.1976; Z. FLUGWISSENSCH.; DTSCH.; DA. 1976; VOL. 24; NO 6; PP. 301-329; ABS. ANGL. FR.; BIBL. 1 P. 1/2Article

A SIMPLE METHOD FOR THE CALIBRATION OF A SUPERSONIC MOLECULAR BEAM SOURCED'ANNA E; LEGGIERI G; CONFORTI G et al.1980; VACUUM; ISSN 0042-207X; GBR; DA. 1980; VOL. 30; NO 3; PP. 121-124; BIBL. 5 REF.Article

ELEVATED-TEMPERATURE EFFECTS ON STRAIN GAGES ON THE YF-12 A WINGJENKINS JM; FIELD RA; SEFIC WJ et al.1979; EXPER. MECH.; USA; DA. 1979; VOL. 19; NO 3; PP. 81-86; BIBL. 12 REF.Article

H II BUBBLES AND SHOCKS IN MOLECULAR CLOUDSMAZUREK TJ.1981; ASTROPHYS. SPACE SCI. LIBR.; ISSN 0067-0057; NLD; DA. 1981; VOL. 93; PP. 61-66; BIBL. 11 REF.Conference Paper

MOTION-BASE SIMULATOR RESULTS OF ADVANCED SUPERSONIC TRANSPORT HANDLING QUALITIES WITH ACTIVE CONTROLSFEATHER JB; JOSHI DS.1981; GUIDANCE AND CONTROL CONFERENCE/1981/ALBUQUERQUE NM; USA; NEW-YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; PP. 274-280; BIBL. 8 REF.Conference Paper

ABRUPT SUPERSONIC MOTION OF A POINT SOURCESHANKARA TS; KAMAL KANTI NANDI.1981; J. ACOUST. SOC. AM.; ISSN 0001-4966; USA; DA. 1981; VOL. 69; NO 5; PP. 1502-1503; BIBL. 2 REF.Article

INTERDICTION ENERGETIQUE DES REGIMES SUPERSONIQUES DU COLLAPSUS DES OSCILLATIONS DE LANGMUIRFRAJMAN GM.1979; PIS'MA ZH. EKSPER. TEOR. FIZ.; SUN; DA. 1979; VOL. 30; NO 9; PP. 557-560; BIBL. 8 REF.Article

Caractéristiques de la combustion supersonique de gaz non mélangés dans un tunnelZIMONT, V. L; LEVIN, V. M; MESHCHERYAKOV, E. A et al.Fizika goreniâ i vzryva. 1983, Vol 19, Num 4, pp 75-78, issn 0430-6228Article

LE PROBLEME DE LA SIMULATION DU PLASMA D'AIR SUR UN TRAJET BALLISTIQUE DANS UN MELANGE D'AIR ET D'UN GAZ LOURDSKURIN LI.1980; Z. TEH. FIZ.; ISSN 0044-4642; SUN; DA. 1980; VOL. 50; NO 4; PP. 858-861; BIBL. 8 REF.Article

ROLLING OF ELASTIC CYLINDERS WITH FRICTION AT SUPERSONIC SPEEDBARBER JR; COMNIOU M.1982; INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES; ISSN 0020-7683; USA; DA. 1982; VOL. 18; NO 9; PP. 783-789; BIBL. 9 REF.Article

SUPERSONIC STELLAR WINDS AND RAPID MASS LOSS IN COOL STARSMULLAN DJ.1978; ASTROPHYS. J.; USA; DA. 1978; VOL. 226; NO 1 PART. 1; PP. 151-166; BIBL. 78 REF.Article

EXPERIMENTS ON SUPERSONIC JET NOISE.LAUFER J; SCHLINKER R; KAPLAN RE et al.1976; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 4; PP. 489-497; BIBL. 22 REF.Article

IMPULSIVE MOTION OF A SPHERE AT SUPERSONIC SPEEDSCHANG SSH.1980; J. FLUIDS ENG.; ISSN 0098-2202; USA; DA. 1980; VOL. 102; NO 1; PP. 41-46; BIBL. 12 REF.Article

AMELIORATION DES PERFORMANCES D'UN ACCELERATEUR ELECTROMAGNETIQUE DE CONDUCTEURSGAL'ETOV VP; IVANOV EN.1979; P.M.T.F.; SUN; DA. 1979; NO 4; PP. 105-108; BIBL. 7 REF.Article

OPTIMAL CONTROL APPLICATION IN SUPERSONIC AIRCRAFT PERFORMANCECHING FANG LIN.1982; IEE PROC., D; ISSN 0143-7054; GBR; DA. 1982; VOL. 129; NO 4; PP. 113-117; BIBL. 3 REF.Article

ACCELERATION ET INTERACTION DES FLUX NON MONOPHASIQUESBLAGOSKLONOV VI; KUZNETSOV VM; LIPATOV II et al.1981; P.M.T.F.; SUN; DA. 1981; NO 3; PP. 18-26; BIBL. 9 REF.Article

LE PROBLEME DE L'INTERACTION D'UN COIN SE DEPLACANT AVEC UNE VITESSE SUPERSONIQUE AVEC LA LIMITE DE SEPARATION DE DEUX GAZTUGAZAKOV R YA.1983; IZVESTIJA AKADEMII NAUK SSSR. MEHANIKA ZIDKOSTI I GAZA; ISSN 0568-5281; SUN; DA. 1983; NO 3; PP. 92-96; BIBL. 7 REF.Article

SOLUTIONS NUMERIQUES DE L'INTERACTION D'UNE ONDE DE CHOC PLANE AVEC DES OBSTACLES AU REPOS OU MOBILES = NUMERICAL SOLUTIONS TO THE INTERACTION OF A PLANAR SHOCKWAVECHAMPNEY JOELLE.1982; ; FRA; DA. 1982; 89 F.; 30 CM; BIBL. 87 REF.; TH. 3E CYCLE: MATH./PARIS 6/1982Thesis