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MOUVEMENT NON STATIONNAIRE D'UN FLUIDE COMPRESSIBLE VISQUEUX DANS UNE COUCHE SPHERIQUEASTAF'EVA NM; BRAILOVSKAYA I YU; YADORSKAYA IM et al.1972; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1972; NO 3; PP. 4-10; BIBL. 12REF.Serial Issue

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

SUBSONIC LOADS ON WINGS HAVING SHARP LEADING EDGES AND TIPS.KANDIL OA; MOOK DT; NAYFEH AH et al.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 1; PP. 62-63; BIBL. 10 REF.Article

FINITE-AMPLITUDE CONVECTION IN A COMPRESSIBLE MEDIUM AND ITS APPLICATION TO SOLAR GRANULATION.VAN DER BORGHT R.1975; MONTH. NOT. R. ASTR. SOC.; G.B.; DA. 1975; VOL. 173; NO 1; PP. 85-95; BIBL. 26 REF.Article

OBLIQUE COMPRESSIBLE SEARS FUNCTION.FILOTAS LT.1974; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 11; PP. 1601-1603; BIBL. 11 REF.Article

ON LIFTING WINGS WITH PARABOLIC TIPS.JORDAN PF.1974; Z. ANGEW. MATH. MECH.; DTSCH.; DA. 1974; VOL. 54; NO 8; PP. 463-477; ABS. ALLEM. RUSSE; BIBL. 17 REF.Article

CALCUL DES CARACTERISTIQUES D'UNE GRILLE EN ECOULEMENT COMPRESSIBLE JUSQU'AU REGIME SUPERCRITIQUE SANS CHOC PAR LA METHODE DES SINGULARITES.LUU TS; COULMY G; GRISSA A et al.1974; ENTROPIE; FR.; DA. 1974; VOL. 10; NO 58; PP. 17-23; ABS. ANGL. ALLEM. ESP.; BIBL. 10 REF.Article

AERODYNAMIQUE SUBSONIQUE D'UN ECOULEMENT LIBRE AUTOUR D'UN CORPS ARBITRAIREKOVAL FF.1976; DOP. AKAD. NAUK UKRAJIN. R.S.R., A; S.S.S.R.; DA. 1976; NO 5; PP. 416-420; ABS. ANGL. RUSSE; BIBL. 8 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

DIAGONAL DOMINANCE AND S.O.R. PERFORMANCE WITH SKEW NETS.O'CARROLL MJ.1976; INTERNATION. J. NUMER. METHODS ENGNG; G.B.; DA. 1976; VOL. 10; NO 1; PP. 225-230; BIBL. 7 REF.Article

MULTIPOINT DISTRIBUTION FUNCTION HIERARCHY FOR COMPRESSIBLE TURBULENT FLOW.FOX RL.1975; PHYS. OF FLUIDS; U.S.A.; DA. 1975; VOL. 18; NO 10; PP. 1245-1248; BIBL. 13 REF.Article

BROWNIAN MOTION AND THE EQUIPARTITION THEOREMBURGESS RE.1973; PHYS. LETTERS, A; NETHERL.; DA. 1973; VOL. 42; NO 5; PP. 395-396; BIBL. 9 REF.Serial Issue

PRESSURE AND VELOCITY DISTRIBUTIONS IN PULSATING LAMINAR PIPE FLOW. = DISTRIBUTIONS DE PRESSION ET DE VITESSE DANS UN ECOULEMENT LAMINAIRE PULSATOIRE EN TUYAUTERIEOHMI M; USUI T; FUKAWA M et al.1976; BULL. J.S.M.E.; JAP.; DA. 1976; VOL. 19; NO 129; PP. 298-306; BIBL. 14 REF.Article

COMPRESSIBLE CONICAL DIFFUSER FLOW USING THE ENERGY DEFICIT BOUNDARY LAYER METHOD.LIVESEY JL; ODUKWE AO; KAMAL WA et al.1975; J. MECH. ENGNG SCI.; G.B.; DA. 1975; VOL. 17; NO 4; PP. 206-213; BIBL. 20 REF.Article

FLOW MEASUREMENT. = MESURE DE DEBITMURDOCK JW; SMITH LT.1975; IN: FUNDAM. AEROSP. INSTRUM. VII. FUNDAM. TEST MEASUR. II. TUTORIAL PROC. 21ST INT. ISA INSTRUM. SYMP.; PHILADELPHIA, PA.; 1975; PITTSBURGH; INSTRUM. SOC. AMERICA; DA. 1975; PP. 59-63; BIBL. 3 REF.Conference Paper

PREDICTION OF RECOVERY FACTOR AND REYNOLDS' ANALOGY FOR COMPRESSIBLE TURBULENT FLOW.GERHART PM.1975; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 7; PP. 966-968; BIBL. 12 REF.Article

INSTATIONAERE DRUCKVERTEILUNGEN AN EINEM HARMONISCH SCHWINGENDEN, GESTAFFELTEN SCHAUFELGITTER. II. ERGEBNISSE FUER KOMPRESSIBLE STROEMUNG. = DISTRIBUTION DE PRESSION INSTATIONNAIRE SUR UNE GRILLE D'AUBES ECHELONNEE EN OSCILLATIONS HARMONIQUES. II. RESULTATS POUR UN ECOULEMENT COMPRESSIBLETRIEBSTEIN H; CARSTENS V; WAGENER J et al.1975; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 58; PP. 1-89; ABS. ANGL.; BIBL. 1 P. 1/2Serial Issue

CALCUL DE L'INTERACTION DE L'ONDE DE CHOC AVEC UN CORPS EMOUSSEGRUDNITSKIJ VG; PROKHORCHUK YU A.1975; CHISLEMN. METODY MEKH. SPLOSHN. SREDY; S.S.S.R.; DA. 1975; VOL. 6; NO 4; PP. 42-55; BIBL. 11 REF.Article

CALCUL DES JETS CUMULATIFSSHURSHALOV LV.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 4; PP. 116-122; BIBL. 7 REF.Article

DEVELOPPEMENT D'UNE INSTABILITE DE TAYLOR DANS DES MILIEUX CONDUCTEURS COMPRESSIBLES EN PRESENCE D'UN CHAMP MAGNETIQUEPOLYANIN AD.1975; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1975; NO 5; PP. 15-19; BIBL. 4 REF.Article

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

ACOUSTIC RADIATION FROM SURFACES OSCILLATING AT LARGE AMPLITUDE AND SMALL MACH NUMBER.FROST PA; HARPER EY.1975; J. ACOUST. SOC. AMER.; U.S.A.; DA. 1975; VOL. 58; NO 2; PP. 318-325; BIBL. 14 REF.Article

AN ANALYSIS OF THE UNSTEADY DISCHARGE PROCESS FROM A CYLINDER.NEILSON JH; CRAWFORD RA.1975; PRACE INST. MASZ. PRZEPHYW.; POLSKA; DA. 1975; VOL. 69; PP. 57-69; ABS. POL. RUSSE; BIBL. 5 REF.Article

COMPRESSIBLE FLOW EJECTORS. II. FLOW FIELD MEASUREMENTS AND ANALYSIS.HEDGES KR; HILL PG.1974; J. FLUIDS ENGNG; U.S.A.; DA. 1974; VOL. 96; NO 3; PP. 282-288; BIBL. 7 REF.Article

MEASUREMENT OF COMPRESSIBLE FLUIDS. DIFFERENT FLOWMETERS CAN GIVE DIFFERENT RESULTS.EVANS HJ.1974; INSTRUM. CONTROL SYST.; U.S.A.; DA. 1974; VOL. 47; NO 2; PP. 61-64Article

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