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BOUNDARY LAYER TRANSITION ON SUPERSONIC CONES IN AN AEROBALLISTIC RANGE.POTTER JL.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 132; PP. 1-13; BIBL. 21 REF.Conference Paper

ANALYSE EXPERIMENTALE ET THEORIQUE DES COUCHES LIMITES TURBULENTES TRIDIMENSIONNELLES DANS UN CANAL SUPERSONIQUE COURBE.COUSTEIX J; MICHEL R.1975; RECH. AEROSPAT.; FR.; DA. 1975; NO 1; PP. 1-10; ABS. ANGL.; BIBL. 2 REF.Article

FINITE ELEMENT SUPERSONIC AERODYNAMICS FOR OSCILLATING PARALLEL WINGS.APPA K; SMITH GCC.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 8; PP. 433-434; BIBL. 11 REF.Article

SUPERSONIC FLIGHT IN A STRATIFIED SHEARED ATMOSPHERE.SIROVICH L; CHONG TH.1974; PHYS. OF FLUIDS; U.S.A.; DA. 1974; VOL. 17; NO 2; PP. 310-320; BIBL. 28 REF.Article

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

EXPERIMENTAL STUDY OF SEPARATION FROM THE BASE OF A CONE AT SUPERSONIC SPEEDS.KAYSER LD; DANBERG JE.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 11; PP. 1607-1609; BIBL. 8 REF.Article

IL-22 : A critical mediator in mucosal host defenseAUJLA, S. J; KOLLS, J. K.Journal of molecular medicine (Berlin. Print). 2009, Vol 87, Num 5, pp 451-454, issn 0946-2716, 4 p.Article

UNSTEADY AERODYNAMICS OF NONPLANAR WINGS AND WING-TAIL CONFIGURATIONS OF ELASTIC FLIGHT VEHICLES IN SUPERSONIC FLIGHT = AERODYNAMIQUE INSTATIONNAIRE D'AILES NON PLANES ET DE CONFIGURATIONS AILE-EMPENNAGE DE VEHICULES ELASTIQUES EN VOL SUPERSONIQUEII JM; ROWE WS.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 1; PP. 19-27; BIBL. 15 REF.Serial Issue

OSCILLATORY SUPERSONIC KERNEL FUNCTION METHOD FOR ISOLATED WINGS.CUNNINGHAM AM JR.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 10; PP. 609-615; BIBL. 15 REF.Article

WIND TUNNEL EXPERIMENTS RELATING TO SUPERSONIC AND HYPERSONIC BOUNDARY LAYER TRANSITION.KENDALL JM.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 133; PP. 1-13; BIBL. 23 REF.Conference Paper

SURFACE FLOWFIELD INDUCED BY THE TURBULENT BOUNDARY LAYER ON A YAWED CONE.MARCILLAT J.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 8; PP. 1164-1165; BIBL. 7 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

CROSS-HATCHING STUDIES. A CRITICAL REVIEW.SWIGART RJ.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 10; PP. 1301-1318; BIBL. 46 REF.Article

A COMPARISON OF THEORETICAL AND EXPERIMENTAL INVESTIGATIONS OF TWO DIFFERENT AXIAL SUPERSONIC COMPRESSORS.SIMON H; BOHN D.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES. PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (15P.); BIBL. 6 REF.Conference Paper

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

LA SOUFFLERIE SUPERSONIQUE DE GRILLE PLANE DE L'ONERA A CHALAIS-MEUDON.MEAUZE G.1975; AERONAUT. ET ASTRONAUT.; FR.; DA. 1975; NO 50; PP. 57-61; ABS. ANGL. ALLEM.; BIBL. 4 REF.Article

SUR L'INFLUENCE DES IMPURETES SUR LE COEFFICIENT DE RENFORCEMENT OPTIQUE LORS DE L'ECOULEMENT DU GAZ DE RELAXATION DANS UNE TUYERE SUPERSONIQUEMAKAROV VN; LOSEV SA.1975; FIZ. GOREM. VYRYVA; S.S.S.S.R.; DA. 1975; VOL. 11; NO 5; PP. 804-806; BIBL. 13 REF.Article

SUPERSOMIC NEUTRAL WINDS IN AN OUTER ATMOSPHERE. I. ISOTHERMAL CONDITIONS.GILBERT NE; COLE KD.1974; AUSTRAL. J. PHYS.; AUSTRAL.; DA. 1974; VOL. 27; NO 4; PP. 511-528; BIBL. 38 REF.Article

EINE GRAPHISH-ANALYTISCHE METHODE ZUR BESTIMMUNG DER OPTIMUM-OPTIMORUM-FORM DES DUENNEN DELTAFLUEGELS IN UEBERSCHALLSTROEMUNG. = METHODE GRAPHO-ANALYTIQUE POUR DETERMINER LA FORME OPTIMALE DE L'AILE DELTA MINCE EN ECOULEMENT SUPERSONIQUENASTASE A.1974; REV. ROUMAINE SCI. TECH., MEC. APPL.; ROUMAN.; DA. 1974; VOL. 19; NO 1; PP. 15-35; BIBL. 7 REF.Article

Welche Kältemittel in der Zukunft? = Which refrigerant in the future?DOÊRING, R.Die Kälte und Klimatechnik. 1990, Vol 43, Num 9, pp 472-482, issn 0343-2246, 6 p.Article

EINFLUSS SCHRAEGER HINTERKRANTEN UND EINFLUSS DES EIGENGEWICHTS DER BESPANNUNG AUF DIE UMSTROEMUNG KONISCHER PARAGLEITER MIT SCHWACHER WOELBUNG IM UEBERSCHALL. = INFLUENCE DES BORDS DE FUITE OBLIQUES ET DU POIDS DU REVETEMENT SUR L'ECOULEMENT AUTOUR DES PARAPLANEURS A FAIBLE COURBURE CONIQUE EN SUPERSONIQUEWAGNER B.1976; Z. FLUGWISSENSCH.; DTSCH.; DA. 1976; VOL. 24; NO 6; PP. 329-340; ABS. ANGL. FR.; BIBL. 8 REF.Article

SIMPLIFIED ANALYSIS OF SUPERSONIC BASE FLOWS INCLUDING INJECTION AND COMBUSTION.SCHETZ JA; BILLIG FS; FAVIN S et al.1976; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 1; PP. 7-8; BIBL. 6 REF.Article

PREDICTION OF ROLL MOMENTS ON FINNED BODIES IN SUPERSONIC FLOW.OBERKAMPF WL.1975; J. SPACECR. ROCK.; U.S.A.; DA. 1975; VOL. 12; NO 1; PP. 17-21; BIBL. 13 REF.Article

CALCUL DES CARACTERISTIQUES AERODYNAMIQUES DES AILES DE GEOMETRIE COMPLEXE EN ECOULEMENT SUPERSONIQUEBOKOVIKOV YU G.1974; IZVEST. SIBIR. OTDEL. AKAD. NAUK S.S.S.R., TEKH. NAUK; S.S.S.R.; DA. 1974; NO 8; PP. 48-55; BIBL. 10 REF.Article

RESOLUTION D'UN PROBLEME VARIATIONNEL RELATIF A LA DETERMINATION DU PROFIL D'UNE TUYERE QUI REALISE UN ECOULEMENT SUPERSONIQUE UNIFORMERYLOV AI.1974; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1974; NO 4; PP. 85-92; BIBL. 12 REF.Article

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