Pascal and Francis Bibliographic Databases

Help

Search results

Your search

kw.\*:("SUBSONIC FLOW")

Document Type [dt]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Publication Year[py]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Discipline (document) [di]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Language

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Author Country

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Origin

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Results 1 to 25 of 2108

  • Page / 85
Export

Selection :

  • and

SUBSONIC AERODYNAMICSDELAURIER JD; REID LD.1978; INST. AEROSPACE STUD., UNIV. TORONTO, ANNU. PROGR. REP.; CAN; DA. 1978; PP. 57-58; BIBL. 7 REF.Article

CARACTERISTIQUES AERODYNAMIQUES DES AILES DELTA POUR DES VITESSES DE VOL SUBSONIQUEVORONIN VI; SHVETS AI.1981; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1981; NO 6; PP. 104-109; BIBL. 10 REF.Article

EXPERIMENTALLY DETERMINED STABILITY PARAMETERS OF A SUBSONIC CASCADE OSCILLATING NEAR STALL.CARTA FO; HILAIRE AOS.1978; J. ENGNG POWER; U.S.A.; DA. 1978; VOL. 100; NO 1; PP. 111-120; BIBL. 8 REF.Article

THE GERMAN-DUTCH LOW SPEED WIND TUNNEL DNW.SEIDEL M; JAARSMA F.1978; AERONAUT. J.; G.B.; DA. 1978; VOL. 82; NO 808; PP. 167-173Article

QUADRATURE FORMULAS FOR CHORDWISE INTEGRALS OF LIFTING SURFACE THEORIESANDO S; ICHIKAWA A.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 3; PP. 466-467; BIBL. 6 REF.Article

ECOULEMENT NON-STATIONNAIRE D'UN GAZ DANS LE VIDE A TRAVERS UNE BARRIERE PERFOREEMILLER LG.1983; PMTF. ZURNAL PRIKLADNOJ MEHANIKI I TEHNICESKOJ FIZIKI; ISSN 0044-4626; SUN; DA. 1983; NO 2; PP. 62-65; BIBL. 3 REF.Article

HIGH-FREQUENCY SUBSONIC FLOW PAST A PULSATING THIN AIRFOIL.PLOTKIN A.1978; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1978; VOL. 16; NO 4; PP. 405-407; BIBL. 8 REF.Article

CARACTERISTIQUES AERODYNAMIQUES D'AILES DELTA A VITESSE SUBSONIQUEVORONIN VI.1983; VESTNIK MOSKOVSKOGO UNIVERSITETA. SERIJA 1: MATEMATIKA, MEHANIKA; ISSN 0579-9368; SUN; DA. 1983; NO 1; PP. 89-91; ABS. ENG; BIBL. 4 REF.Article

AERODYNAMICS OF WRAP-AROUND FINSBAR HAIM B; SEGINER A.1982; ISRAEL ANNUAL CONFERENCE ON AVIATION AND ASTRONAUTICS. 24/1982-02-17/TEL-AVIV, HAIFA; ISR; HAIFA: IMPR. AYALON OFFSET; DA. 1982; PP. 79-86; BIBL. 15 REF.Conference Paper

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

EFFECTS OF FREE-STREAM TURBULENCE ON DIFFUSER PERFORMANCEHOFFMANN JA.1981; J. FLUIDS ENG.; ISSN 0098-2202; USA; DA. 1981; VOL. 103; NO 3; PP. 385-390; BIBL. 23 REF.Article

OPTIMIERUNG DES RELAXATIONS WIDERSTANDS SCHLANKER PROFILANOZOLNUNGEN IN STATIONAERER UNTERSCHALLSTROEMUNG. II: DUERE UND FLUEGELGITTER = OPTIMISATION DE LA RESISTANCE A LA RELAXATION DE PROFILS MINCES EN ARRANGEMENTS DANS UN ECOULEMENT SUBSONIQUE INSTATIONNAIRE. II: TUYERE ET CASCADE DE PROFILSSCHILLING H.1980; Z. FLUGWISSENSCH. WELTR.-FORSCH.; DEU; DA. 1980; VOL. 4; NO 4; PP. 209-216; ABS. ENG; BIBL. 17 REF.Article

MODELLING LOW MACH NUMBER NOISEMOEHRING W.1979; MECHANICS OF SOUND GENERATION IN FLOWS. SYMPOSIUM/1979/GOETTINGEN; DEU/USA; BERLIN: SPRINGER-VERLAG/HEIDELBERG: SPRINGER-VERLAG/NEW YORK: SPRINGER-VERLAG; DA. 1979; PP. 85-96; BIBL. 13 REF.Conference Paper

APPLICATION OF LAMINAR FLOW CONTROL TO LARGE SUBSONIC MILITARY TRANSPORT AIRPLANESJOBE CE; KULFAN RM; VACHAL JD et al.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-95; 14 P.; BIBL. 4 REF.Conference Paper

EXPERIMENTAL DETERMINATION OF IMPROVED AERODYNAMIC CHARACTERISTICS UTILIZING BIPLANE WING CONFIGURATIONS.OLSON EC; SELBERG BP.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 4; PP. 256-261; BIBL. 11 REF.Article

SUBSONIC AXISYMMETRIC NEAR-WAKE STUDIESMERZ RA; PAGE RH; PRZIREMBEL CEG et al.1978; A.I.A.A.J., NEW YORK; USA; DA. 1978; VOL. 16; NO 7; PP. 656-662; BIBL. 25 REF.Article

LOW-FREQUENCY APPROXIMATIONS IN UNSTEADY SMALL PERTURBATION SUBSONIC FLOWS.AMIET RK.1976; J. FLUID MECH.; G.B.; DA. 1976; VOL. 75; NO 3; PP. 545-552; BIBL. 16 REF.Article

AERODYNAMIQUE DES VITESSES HYPOSONIQUES (ECOULEMENTS A PETITS NOMBRES DE MACH)ZEJTUNYAN R KH.1983; PMTF. ZURNAL PRIKLADNOJ MEHANIKI I TEHNICESKOJ FIZIKI; ISSN 0044-4626; SUN; DA. 1983; NO 2; PP. 53-61; BIBL. 27 REF.Article

DOUBLET LATTICE METHOD-SCHEMES FOR CPU TIME REDUCTIONSIMHA PRASAD DS; HOLLA VS.1980; COMPUTER METHODS APPL. MECH. ENGNG; NLD; DA. 1980; VOL. 23; NO 1; PP. 59-65; BIBL. 4 REF.Article

A ONE-DIMENSIONAL ANALYSIS AND PERFORMANCE PREDICTION OF SUBSONIC RADIAL TURBINESHAMAJIMA M.1980; BULL. JSME; ISSN 0021-3764; JPN; DA. 1980; VOL. 23; NO 186; PP. 2064-2070; BIBL. 14 REF.Article

LIFTING SURFACE THEORY FOR SKEWED AND SWEPT SUBSONIC WINGSFRINK NT.1979; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS. ANNUAL MEETING AND TECHNICAL DISPLAY. 15/1979/WASHINGTON DC; USA; NEW YORK: AIAA; DA. 1979; VOL. 551; PP. 1-10; BIBL. 11 REF.Conference Paper

COMPUTER MODEL OF A FULLY DEPLOYED PARACHUTE.TORY C; AYRES R.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 7; PP. 675-679; BIBL. 5 REF.Article

REYNOLDS NUMBER EFFECTS ON BOATTAIL DRAG OF WING-BODIES.REUBUSH DE.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 5; PP. 455-459; BIBL. 18 REF.Article

SUR LE CALCUL DES ECOULEMENTS SUBSONIQUES D'UN GAZ VISQUEUX DANS L'APPROXIMATION DES EQUATIONS GENERALISEES DE PRANDTLPROKHUR NZ.1977; DINAM. SPLOSHN. SREDY; S.S.S.R.; DA. 1977; VOL. 30; PP. 112-121; BIBL. 4 REF.Article

A NOVEL CONCEPT FOR SUBSONIC INLET BOUNDARY-LAYER CONTROL.MILLER BA.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 4; PP. 403-404; BIBL. 6 REF.Article

  • Page / 85