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Results 1 to 25 of 783

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THE GENERATION OF SOUND BY AERODYNAMIC SOURCES IN AN INHOMOGENEOUS STEADY FLOW.HOWE MS.1975; J. FLUID MECH.; G.B.; DA. 1975; VOL. 67; NO 3; PP. 597-610; BIBL. 19 REF.Article

DISCRETE TONES OF ISOLATED AIRFOILS.TAM CKW.1974; J. ACOUST. SOC. AMER.; U.S.A.; DA. 1974; VOL. 55; NO 6; PP. 1173-1177; BIBL. 11 REF.Article

NOISE CAUSED BY THE INTERACTION OF A ROTOR WITH ANISOTROPIC TURBULENCEKERSCHEN EJ; GLIEBE PR.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 6; PP. 717-723; BIBL. 23 REF.Article

SPECTRAL BROADENING EFFECTS IN OPEN WIND TUNNELS IN RELATION TO NOISE ASSESSMENTROSS R.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 5; PP. 567-572; BIBL. 9 REF.Article

RATIONAL FUNCTION REPRESENTATION OF FLAP NOISE SPECTRA INCLUDING CORRECTION FOR REFLECTION EFFECTS.MILES JH.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 193; PP. 1-24; H.T. 6; BIBL. 2 P. 1/2Conference Paper

ANALYSIS OF ACOUSTIC RADIATION IN A JET FLOW ENVIRONMENT.MUNGUR P; PLUMBLEE HE; DOAK PE et al.1974; J. SOUND VIBRAT.; G.B.; DA. 1974; VOL. 36; NO 1; PP. 21-52; BIBL. 20 REF.Article

SOUND SOURCES IN AERODYNAMICS: FACT AND FICTIONFFOWCS WILLIAMS JE.1981; AEROSPACE SCIENCES MEETING. 19 /1981-01-12/SAINT LOUIS MO; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; 11 P.; BIBL. 15 REF.Conference Paper

THE USE OF A ROTATING ARM FACILITY TO STUDY FLIGHT EFFECTS ON JET NOISE.SMITH W.sdIN: 2ND INT. SYMP. AIR BREATHING ENGINES, PROC.; SHEFFIELD, ENGL.; 1974; LONDON; R. AERONAUT. SOC.; DA. S.D.; PP. (13P.)Conference Paper

UEBERLEGUNGEN ZUM PROJEKT EINES AEROAKUSTIK-WINDKANALS. = CONSIDERATIONS SUR LE PROJET DE SOUFFLERIE AEROACOUSTIQUESCHULZ G.1974; DTSCHE LUFT-U. RAUMFAHRT, MITT.; DTSCH.; DA. 1974; NO 74-27; PP. 1-18; ABS. ANGL.; BIBL. 4 REF.Article

ACOUSTIC OSCILLATIONS IN INTERNAL CAVITY FLOWS: NONLINEAR RESONANT INTERACTIONSISAACSON L; MARSHALL AG.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 20; NO 1; PP. 152-154; BIBL. 12 REF.Article

BRUIT D'ORIGINE AERODYNAMIQUELEGENDRE R.1980; C.R. HEBD. SEANCES ACAD. SCI., SER. B; ISSN 0302-8437; FRA; DA. 1980; VOL. 290; NO 13; PP. 313-315; ABS. ENG; BIBL. 2 REF.Article

DERIVATION OF THE FUNDAMENTAL EQUATION OF SOUND GENERATED BY MOVING AERODYNAMIC SURFACESAGGARWAL HR.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 7; PP. 1048-1050; BIBL. 6 REF.Article

LOW NOISE LEVEL NOZZLES AND EXHAUST SILENCERS FOR QUIETING AIR DISCHARGESALERNO CM.1975; IN: INTER-NOISE 75. INT. CONF. NOISE CONTROL ENG. PROC.; SENDAI; 1975; SENDAI; TOHOKU UNIV.; DA. 1975; PP. 679-682; BIBL. 4 REF.Conference Paper

DISCRETE TONES OF ISOLATED AIRFOILSTAM CKW.1974; J. ACOUST. SOC. AMER.; U.S.A.; DA. 1974; VOL. 55; NO 6; PP. 1173-1177; BIBL. 11 REF.Article

EFFECT OF CONFIGURATION VARIATION ON EXTERNALLY BLOWN FLAP NOISE.DORSCH RG; GOODYKOONTZ JH; SARGENT NB et al.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 190; PP. 1-19; H.T. 13; BIBL. 2 P.Conference Paper

SPECTRUM OF ROTOR NOISE CAUSED BY ATMOSPHERIC TURBULENCEHANSON DB.1974; J. ACOUST. SOC. AMER.; U.S.A.; DA. 1974; VOL. 56; NO 1; PP. 110-126; BIBL. 24 REF.Article

DISQUE A TROUS MULTIPLES UTILISE POUR LA SUPPRESSION DU BRUIT DE SORTIEJUNGOWSKI WM; SZUMOWSKI AP.1974; ARCH. AKUST.; POLSKA; DA. 1974; VOL. 9; NO 3; PP. 339-359; ABS. RUSSE ANGL.; BIBL. 1 P.Article

COEFFICIENT DE REMPLISSAGE DES OUVERTURES DANS LE ROTOR D'UNE SIRENE DYNAMIQUEYUDAEV VF.1979; IZVEST. VYSSH. UCHEBN. ZAVED., MASH.-STR.; SUN; DA. 1979; NO 4; PP. 96-100; BIBL. 2 REF.Article

CORRELATION ON JET NOISE DATA IN TERMS OF A SELF NOISE-SHEAR NOISE MODEL. = CORRELATION SUR LES DONNEES DE BRUIT DE JET D'APRES UN MODELE BRUIT PROPRE-BRUIT DE CISAILLEMENTNOSSEIR NSM.1975; U.T.I.A.S. TECH. NOTE; CANADA; DA. 1975; NO 193; PP. (23P.); H.T. 20; BIBL. 1 P.Article

APPLICATION DE LA TRANSFORMATION AMPLITUDE-FREQUENCE A LA LUTTE CONTRE LE BRUIT AERODYNAMIQUEKOLOTILOV NN; YAROV VN.1975; IN: AKUST. AEHRODIN. ISSLED.; MOSKVA; NAUKA; DA. 1975; PP. 46-56; BIBL. 6 REF.Book Chapter

INVESTIGATION OF ACOUSTIC EFFECTS OF LEADING-EDGE SERRATIONS ON AIRFOILS = RECHERCHES CONCERNANT LES EFFETS ACOUSTIQUES SUR LES PROFILS DE BORDS D'ATTAQUE DENTELESHERSH AS; SODERMAN PT; HAYDEN RE et al.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 4; PP. 197-202; BIBL. 15 REF.Article

UNIFIED APPROACH TO AERODYNAMIC SOUND GENERATION IN THE PRESENCE OF SOLID BOUNDARIESGOLDSTEIN M.1974; J. ACOUST. SOC. AMER.; U.S.A.; DA. 1974; VOL. 56; NO 2; PP. 497-509; BIBL. 20 REF.Article

AERODYNAMIC DESIGN OF A ROTOR BLADE FOR MINIMUM NOISE RADIATION.KARAMCHETI K; YU YH.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 7TH FLUID PLASMA DYN. CONF.; PALO ALTO, CALIF.; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 571; PP. 1-6; BIBL. 8 REF.Conference Paper

AEROSONIC GAMES WITH THE AID OF CONTROL ELEMENTS AND EXTERNALLY GENERATED PULSESPOLDERVAART LJ WIJNANDS APJ; BRONKHORST L.1974; A.G.A.R.D. CONF. PROC.; FR.; DA. 1974; NO 131; PP. 20.1-20.4; BIBL. 3 REF.; (FLUID DYN. PANEL SPEC. MEET.; BRUSSELS; 1973)Conference Paper

EXHAUST VENT SILENCER DESIGN = CONCEPTION D'UN SILENCIEUX DE TUBULURE DE SORTIEMEADOR CL; ALLAN JJ III.1972; J. ENGNG INDUSTRY; U.S.A.; DA. 1972; VOL. 94; NO 4; PP. 1007-1019; BIBL. 21 REF.Serial Issue

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