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Results 1 to 25 of 5350

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COMPRESSIBILITY EFFECTS ON PARACHUTE TRANSIENT PRESSURESKLIMAS PC.1978; J. AIRCR.; USA; DA. 1978; VOL. 15; NO 10; PP. 702-704; BIBL. 3 REF.Article

COMPRESSIBLE FLOW THROUGH A BUTTERFLY THROTTLE VALVE IN A PIPEWOODS WA; GOH GK.1979; PROC. INST. MECH. ENG.; ISSN 0020-3483; GBR; DA. 1979-06; VOL. 193; PP. 237-244; BIBL. 3 REF.Article

CLOSED-FORM SOLUTION OF MODE PROPAGATION IN A NON-UNIFORM CIRCULAR DUCTCHO YC; INGARD KU.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 20; NO 1; PP. 39-44; BIBL. 10 REF.Article

COMPRESSIBILITY EFFECTS ON DYNAMIC STALL OF AN NACA 0012 AIRFOILSANKAR NL; TASSA Y.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 5; PP. 557-558; BIBL. 4 REF.Article

PREDICTION OF THE COMPRESSIBLE VORTEX WAKE FOR BODIES AT HIGH INCIDENCESHIVANANDA TP; OBERKAMPF WL.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 15 P.; BIBL. 22 REF.Conference Paper

QUASI THREE-DIMENSIONAL ANALYSIS OF COMPRESSIBLE FLOW IN CENTRIFUGAL IMPELLERMURATA S; MIYAKE Y; OGAWA T et al.1980; TECHNOL. REP., OSAKA UNIV.; ISSN 0030-6177; JPN; DA. 1980; VOL. 30; NO 1551-1582; PP. 519-526; BIBL. 13 REF.Article

ONE-DIMENSIONAL ANALYSIS OF AIR FLOW THROUGH A SUPERSONIC-SUBSONIC DIFFUSER.TARNOGRODZKI A.1977; ARCH. BUDOWY MASZ.; POLSKA; DA. 1977; VOL. 24; NO 2; PP. 311-317; ABS. POL. RUSSE; BIBL. 2 REF.Article

A NEW LOOK AT THE IONOSPHERE OF JUPITER IN LIGHT OF THE UVS OCCULTATION RESULTSMCCONNELL JC; HOLBERG JB; SMITH GR et al.1982; PLANET. SPACE SCI.; ISSN 0032-0633; GBR; DA. 1982; VOL. 30; NO 2; PP. 151-167; BIBL. 52 REF.Article

ETUDE DES DIFFUSEURS RADIAUX AVEC ECOULEMENT TOURBILLONNAIREVOLOV VT; SHAKHOV VG.1978; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; SUN; DA. 1978; VOL. 21; NO 3; PP. 148-150; BIBL. 3 REF.Article

ON A CLASS OF ATMOSPHERES OCCURRING IN STELLAR HYDRODYNAMIC THEORYADAM JA.1982; ZEITSCHRIFT FUER ANGEWANDTE MATHEMATIK UND PHYSIK; ISSN 0044-2275; CHE; DA. 1982; VOL. 33; NO 4; PP. 473-486; ABS. FRE; BIBL. 7 REF.Article

FINITE-AMPLITUDE CONVECTION IN A COMPRESSIBLE MEDIUM AND ITS APPLICATION TO SUPERGRANULATIONVAN DER BORGHT R.1979; MONTH. NOT. R. ASTR. SOC.; GBR; DA. 1979; VOL. 188; NO 3; PP. 615-624; BIBL. 16 REF.Article

CERTAIN PROPERTIES OF NUMERICAL SCHEMES USED TO SOLVE THE BLADE TO-BLADE FLOW PROBLEM.DESHPANDE RB.1978; INTERNATION. J. NUMER. METHODS ENGNG; G.B.; DA. 1978; VOL. 12; NO 1; PP. 84-92; BIBL. 11 REF.Article

NUMERICAL SOLUTIONS OF THE COMPRESSIBLE HODOGRAPH EQUATION.LIU SK; CHOW WL.1978; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1978; VOL. 16; NO 2; PP. 188-189; BIBL. 7 REF.Article

ANALYTICAL THEORY OF THREE DIMENSIONAL FLOUR IN CENTRIFUGAL COMPRESSORSBOSMAN C.1982; J. MECH. ENG. SCI.; ISSN 0022-2542; GBR; DA. 1982; VOL. 23; NO 4; PP. 179-191; BIBL. 17 REF.Article

ON NONLOCAL DIFFUSION OF GASES.DEMIRAY H; ERINGEN AC.1978; ARCH. MECH.; POLAND; DA. 1978; VOL. 30; NO 1; PP. 65-77; ABS. POL. RUSSE; BIBL. 12 REF.Article

BERECHNUNGSVERFAHREN FUER SCHAUFELGITTER BEI KOMPRESSIBLER STROEMUNG = METHODE DE CALCUL DES GRILLES D'AUBES DANS LES ECOULEMENTS COMPRESSIBLESCZIBERE T.1978; PUBL. TECH. UNIV. HEAVY INDUSTRY, D; HUN; DA. 1978; VOL. 33; NO 2; PP. 71-87; ABS. ENG/RUS; BIBL. 3 REF.Article

STABILITE DE LA DISCONTINUITE TANGENTIELLE DANS DES MILIEUX DISPERSIFSTSVELODUB O YU.1976; IN: NEK. ZADACHI GIDRODIN. TEPLOOBMENA. NAUCHN. KONF. 9. MATER.; NOVOSIBIRSK; 1975; NOVOSIBIRSK; INST. TEPLOFIZ.; DA. 1976; PP. 195-201; BIBL. 7 REF.Conference Paper

A WING-JET INTERACTION THEORY FOR USB CONFIGURATIONS.LAN CE; CAMPBELL JF.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 9; PP. 718-726; BIBL. 20 REF.Article

COMPRESSIBLE HELICOIDAL SURFACE THEORY FOR PROPELLER AERODYNAMICS AND NOISEHANSON DB.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 6; PP. 881-889; BIBL. 30 REF.Article

HYDROMAGNETIC GRAVITATIONAL INSTABILITY OF AN INFINITE CYLINDER OF A COMPRESSIBLE FLUIDSHIVAMOGGI BK.1982; ASTROPHYS. SPACE SCI.; ISSN 0004-640X; NLD; DA. 1982; VOL. 86; NO 2; PP. 371-376; BIBL. 4 REF.Article

THE FLOW OF AN INFINITE COMPRESSIBLE FLUID PAST A RIGID, GRAVITATING SPHERE AND INTERACTING DEGENERATE STAR-RED GIANT BINARIESSHARA MM; SHAVIV G.1980; ASTROPHYS. SPACE SCI.; NLD; DA. 1980; VOL. 67; NO 2; PP. 427-443; BIBL. 19 REF.Article

CALCULATION OF THE BLADE-TO-BLADE COMPRESSIBLE FLOW FIELD IN TURBO-IMPELLERS USING THE FINITE-ELEMENT METHOD.ADLER D; KRIMERMAN Y.1977; J. MECH. ENGNG SCI.; G.B.; DA. 1977; VOL. 19; NO 3; PP. 108-112; BIBL. 15 REF.Article

COMPRESSIBLE BOUNDARY-LAYER STABILITY CALCULATIONS FOR SWEPTBACK USINGS WITH SUCTIONMACK LM.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 3; PP. 363-369; BIBL. 18 REF.Article

SKIN FRICTION AND HEAT TRANSFER AT AN INFINITE SWEPT ATTACHMENT LINEPOLL DIA.1981; AERONAUT. Q.; ISSN 0001-9259; GBR; DA. 1981; VOL. 32; NO 4; PP. 299-318; BIBL. 26 REF.Article

STABILITY ANALYSIS OF SLOW SPHERICAL MOTION FOR A GRAVITATING FLUIDLIVIO M; BUCHLER JR; PESNELL WD et al.1981; ASTROPHYS. J.; ISSN 0004-637X; USA; DA. 1981; VOL. 243; NO 2; PART. 1; PP. 617-624; BIBL. 16 REF.Article

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