COMMANDE EN TEMPS REEL DU NOMBRE DE MACH DANS UNE SOUFFLERIE TRANSSONIQUE A RAFALES.GOBERT JL.1975; OFF. NATION. ET. RECH. AEROSPAT., NOTE TECH.; FR.; DA. 1975; PP. 1-66; ABS. ANGL.; BIBL. 20 REF.; (THESE DOCT. 3E CYCLE; PARIS VI; 1975)Thesis

CALCULATING STARTING TIMES FOR SUPERSONIC NOZZLE UPSTREAM OF A DIAPHRAGM. = CALCUL DES TEMPS DE DEMARRAGE POUR UNE TUYERE SUPERSONIQUE EN AMONT D'UN DIAPHRAGMEBARBOUR NM; IMRIE BW.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 10; PP. 1394-1396; BIBL. 5 REF.Article

ECOULEMENT SYMETRIQUE SANS DECOLLEMENT D'UN FLUX TRANSSONIQUE SUR DES CORPS CYLINDRO-CONIQUESBACHMANOVA NS; KIRNASOV BS; KUDRYAVTSEV VV et al.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 6; PP. 164-167; BIBL. 2 REF.Article

DER EINFLUSS DER LUFTVORKUEHLUNG VOR DER VERDICHTUNG BEI LUFTATMENDEN ANTRIEBEN EINES RAUMFAHRZEUGTRAEGERS = L'INFLUENCE DU PRE-REFROIDISSEMENT DE L'AIR ASPIRE AVANT LA COMPRESSION DANS LE LANCEUR D'UN VEHICULE SPATIALKUNKLER H.sdIN: 5. JAHRESTAG. DTSCH. GES. LUFT RAUMFAHRT; BERLIN; 1972; S.L.; DA. S.D.; PP. 1-18; H.T. 11; BIBL. 6 REF.Conference Paper

DEFLEXION D'UN ECOULEMENT SUPERSONIQUE AUTOUR D'UNE PLAQUEOVCHINNIKOVA TI; GOLUBITSKAYA RM.1975; VEST. LENINGRAD. UNIV.; S.S.S.R.; DA. 1975; NO 7; PP. 104-109; ABS. ANGL.; BIBL. 4 REF.Article

STUDIO DEI PROFILI ALARI AD ARCO DI CERCHIO CON NUMERO DI MACH ASINTOTICO CRITITCO. III. = ETUDE DES PROFILS D'AILE EN ARC DE CERCLE A NOMBRE DE MACH ASYMPTOTIQUE CRITIQUE. IIILOIODICE R.1974; ATTI ACCAD. SCI. TORINO, CL. SCI. FIS. MAT. NAT.; ITAL.; DA. 1974; VOL. 108; NO 3-4; PP. 445-454; BIBL. 11 REF.Article

EXTENSION OF PERTURBATION SERIES BY COMPUTER: SYMMETRIC SUBSONIC POTENTIAL FLOW PAST A CIRCLE.HOFFMAN GH.1974; J. MEC.; FR.; DA. 1974; VOL. 13; NO 3; PP. 433-447; ABS. FR.; BIBL. 20 REF.Article

SECOND ORDER SUBSONIC SOLUTION FOR A CORRUGATED CIRCULAR CYLINDER IN A CLOSED THROAT WIND TUNNEL.KANSARI HALDER.1975; BULL. CALCUTTA MATH. SCI.; INDIA; DA. 1975; VOL. 67; NO 1; PP. 37-46; BIBL. 13 REF.Article

SOME CHARACTERISTICS OF AIRFOIL-JET INTERACTION WITH MACH NUMBER NONUNIFORMITY.LAN CE.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 8; PP. 491-494; BIBL. 5 REF.Article

SOME EFFECTS ON CONICAL DIFFUSER PERFORMANCE OF PRECEDING NORMAL SHOCK BOUNDARY-LAYER INTERACTION.LIVESEY JL; ODUKWE AO.1974; INSTITUT. MECH. ENGRS, PROC.; G.B.; DA. 1974; VOL. 188; NO 56; PP. 607-613; BIBL. 9 REF.Article

THE INFLUENCE OF REYNOLDS NUMBER ON THE PERFORMANCE OF LOW MACH NUMBER, RADIAL OPEN IMPELLER.FISCHER U; ILBERG H.1973; ISRAEL J. TECHNOL.; ISRAEL; DA. 1973; VOL. 11; NO 6; PP. 373-384; BIBL. 21 REF.Article

VISUALISATION PAR HOLOGRAPHIE ULTRA-RAPIDE DU RELIEF D'UN SILLAGE DE PROJECTILE EN VOL A MACH 2.FAGOT H; SMIGIELSKI P; SIMON G et al.1974; ISL-CO-17-74; FR.; DA. 1974; ABS. ANGL.; BIBL. 3 REF.; (11E CONGR. INT. PHOTOGR. ULTRA-RAPIDE; LONDRES; 1974)Conference Proceedings

A VARIATIONAL FORMULATION OF THE COMPRESSIBLE THROUGHFLOW PROBLEM.OATES GC; KNIGHT CJ; CAREY GF et al.1975; IN: GAS TURBINE CONF. PROD. SHOW; HOUSTON, TEX.; 1975; NEW YORK; AM. SOC. MECH. ENG.; DA. 1975; VOL. 75-GT-32; PP. 1-8; BIBL. 7 REF.Conference Paper

EFFECTS OF REYNOLDS NUMBER ON SWEPT-WING-BODY CONFIGURATIONS WITH HIGH LIFT DEVICES AT TRANSONIC SPEEDS.ATRAGHJI E; SORENSEN H.1974; IN: 9TH CONGR. INT. COUNC. AERONAUT. SCI. PROC.; HAIFA; 1974; JERUSALEM; WEIZMANN SCI. PRESS ISR.; DA. 1974; VOL. 1; PP. 94-120; BIBL. 8 REF.Conference Paper

EIN BEITRAG ZUR WEITERENTWICKLUNG VON PULSATIONSTRIEBWERKEN = CONTRIBUTION AU PERFECTIONNEMENT DES PULSO-REACTEURSHEISE G.1973; Z. FLUGWISSENCH.; DTSCH.; DA. 1973; VOL. 21; NO 6; PP. 189-195; ABS. ANGL. FR.; BIBL. 13 REF.Serial Issue

COMMANDE EN TEMPS REEL DU NOMBRE MACH DANS UNE SOUFFLERIE TRANSSONIQUE A RAFALES.GOBERT JL.1975; ; S.L.; DA. 1975; PP. 1-66; BIBL. 20 REF.; (THESE DOCT. 3E CYCLE SPEC. AUTOM.; PARIS VI)Thesis

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

COMPARISON OF SONIC BOOM MINIMIZATION RESULTS IN REAL AND ISOTHERMAL ATMOSPHERES = COMPARAISON DES RESULTATS DE LA MINIMISATION DU BANG SONIQUE DANS DES ATMOSPHERES REELLES ET ISOTHERMESDARDEN CM.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 5; PP. 496-497; BIBL. 4 REF.Article

EFFECT OF THE MACH NUMBER TEMPERATURE FACTOR ON HEAT TRANSFER FROM A GAS TO A TURBINE BLADE. = INFLUENCE DU FACTEUR TEMPERATURE DU NOMBRE DE MACH SUR LE TRANSFERT DE CHALEUR D'UN GAZ A UNE AUBE DE TURBINEDYBAN YP; GLUSHCHENKO VG.1975; HEAT TRANSFER, SOVIET RES.; U.S.A.; DA. 1975; VOL. 7; NO 2; PP. 17-21; BIBL. 8 REF.Article

LOW SUPERSONIC, THREE-DIMENSIONAL FLOW ABOUT A HEMISPHERE-CYLINDER.TSUYING HSIEH.1975; IN: ANN. INST. AERONAUT. ASTRONAUT. 8TH FLUID PLASMA DYN. CONF.; HARTFORD, CONN.; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 836; PP. 1-9; BIBL. 11 REF.Conference Paper

ANTISYMMETRICALLY CAMBERED AND TORSIONED DELTA WINGS WITH FINITE VELOCITIES AT THE LEADING EDGES.CARAFOLI E; STAICU S.1975; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROUMAN.; DA. 1975; VOL. 20; NO 2; PP. 163-177; BIBL. 7 REF.Article

OSCILLATION PHENOMENA OF PSEUDO-SHOCK WAVES.IKUI T; MATSUO K; NAGAI M et al.1974; BULL. J.S.M.E.; JAP.; DA. 1974; VOL. 17; NO 112; PP. 1278-1285; BIBL. 9 REF.Article

AERODYNAMIC FORCES AND MOMENTS ON A SLENDER WITH A JET PLUME FOR ANGLES OF ATTACK UP TO 180 DEGREES.FLEEMAN EL; NELSON RC.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 110; PP. 1-15; BIBL. 25 REF.Conference Paper

BOUNDARY-LAYER EFFECT IN PANEL FLUTTER.GOLDSTEIN ME.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 9; PP. 1247-1249; BIBL. 7 REF.Article

A THEORETICAL AND EXPERIMENTAL STUDY OF A JET STRETCHER SYSTEMBAUER RC; MATKINS EH; BAREBO RL et al.sdIN: AIAA 7TH AERODYN. TEST. CONF. PALO ALTO, CALIF., 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; NO 993; PP. 1-16; BIBL. 3 REF.Conference Paper