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ETUDE DU COMPORTEMENT DES PLAQUES ET DES COQUES, BASEE SUR LES EQUATIONS INTEGRO-DIFFERENTIELLES DE L'AEROELASTICITE NON STATIONNAIREBELOTSERKOVSKIJ SM; VOL'MIR AS; PONOMAREV AT et al.1974; IZVEST. AKAD. NAUK S.S.S.R., MEKH. TVERD. TELA; S.S.S.R.; DA. 1974; NO 6; PP. 85-94; BIBL. 5 REF.Article

PREDICTION OF ELASTIC-AIRPLANE LONGITUDINAL DYNAMICS FROM RIGID-BODY AERODYNAMICS.SWAIM RL; FULLMAN DG.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 9; PP. 868-873; BIBL. 7 REF.Article

JAHRBUCH 1976. II DER DEUTSCHEN BESSELSCHAFT FUER LUFT- UND RAUMFAHRT E.V. (DGLR). = ANNUAIRE 1976 DE LA SOCIETE ALLEMANDE D'AERONAUTIQUE ET D'AEROSPATIALE (DGLR) III1976; JB. DTSCH. GESELLSCH. LUFT-U. RAUMFAHRT; DTSCH.; DA. 1976; VOL. 3; PP. (381P.); H.T. 76; BIBL. DISSEM.Serial Issue

AEROELASTICITE DE STRUCTURES COMME EFFET DYNAMIQUE D'ORDRE LE PLUS ELEVESPRINC J.1974; STAVEB. CAS.; CESKOSL.; DA. 1974; VOL. 22; NO 10; PP. 637-649; ABS. RUSSE ANGL.; BIBL. 4 REF.Article

A NEW FREQUENCY PARAMETER FOR UNSTEADY AERODYNAMICSANTHONY SR; MYERS MR.1981; STRUCTURES, STRUCTURAL DYNAMICS AND MATERIALS CONFERENCE. 22. AMERICAN INSTITUTE OF AERONAUTICS DYNAMICOSPECIALISTS CONFERENCE/1981/ATLANTA GA; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; PP. 730-732; BIBL. 4 REF.Conference Paper

SYMPOSIUM INTERNATIONAL SUR L'AEROELASTICITE DES TURBOMACHINESSTEPANOV G YU.1977; IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; S.S.S.R.; DA. 1977; NO 5; PP. 197-200Article

MINIMIERUNG DES RELAXATIONSWIDERSTANDES SCHLANKER PROFILE IN FAST GEFRORENER UNTERSCHALLSTROEMUNG = MINIMISATION DE LA RESISTANCE A LA RELAXATION DES PROFILS MINCES DANS UN ECOULEMENT SUBSONIQUE PRES DES CONDITIONS DE GELSCHILLING H.1979; Z. ANGEW. MATH. MECH.; DDR; DA. 1979; VOL. 59; NO 5; PP. T259-T260; BIBL. 5 REF.Article

SOME OBSERVATIONS ON FOUR CURRENT SUBJECTS RELATED TO AEROELASTIC STABILITYASHLEY H.1978; ISRAEL J. TECHNOL.; ISR; DA. 1978; VOL. 16; NO 1-2; PP. 3-22; BIBL. 63 REF.Conference Paper

EFFECT OF MODIFIED AERODYNAMIC STRIP THEORIES ON ROTOR BLADE AEROELASTIC STABILITY.FRIEDMANN P; YUAN C.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 7; PP. 932-940; BIBL. 24 REF.Article

LEADING-EDGE VORTEX EFFECT ON THE FLUTTER SPEED.STARK VJE.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 9; PP. 921-922; BIBL. 7 REF.Article

UNSTEADY AIRLOADS IN SEPARATED AND TRANSONIC FLOW. AGARD STRUCTURES AND MATERIALS PANEL. MEETING. 44; LISBON; 1977.1977; A.G.A.R.D. CONF. PROC.; FR.; DA. 1977; NO 226; PP. (256P.); BIBL. DISSEM.Conference Paper

ADVANCES IN TECHNIQUES FOR DETERMINING THE AEROELASTIC CHARACTERISTICS OF SUSPENSION BRIDGES.RICHARDSON JR.1977; IN: INT. CONF. WIND EFFECTS ON BUILD. AND STRUCT. 4. PROC.; HEATHROW; 1975; CAMBRIDGE; CAMBRIDGE UNIV. PRESS; DA. 1977; PP. 251-277 (15P.); BIBL. 7 REF.Conference Paper

AEROELASTIC STABILITY OF THE 747/ORBITER.REDING JP; ERICSSON LE.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 10; PP. 988-993; BIBL. 14 REF.Article

NOUVEAUX ASPECTS DU PROBLEME DE L'AEROELASTICITE DE TURBOMACHINESOL'SHTEJN LE.1976; PROBL. PROCHN., U.S.S.R.; S.S.S.R.; DA. 1976; NO 3; PP. 3-7Article

ACTIVE FLUTTER SUPPRESSION USING TRAILING-EDGE AN TAB CONTROL SURFACES.NISSIM E.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 6; PP. 757-762; BIBL. 2 REF.Article

VIBRATION ANALYSIS OF ROTOR BLADES WITH PENDULUM ABSORBERSMURTHY VR; HAMMOND CE.1981; J. AIRCR.; ISSN 0021-8669; USA; DA. 1981; VOL. 18; NO 1; PP. 23-29; BIBL. 8 REF.Article

WIND TUNNEL EVALUATION OF AEROELASTICALLY CONFORMABLE ROTORSBLACKWELL RH; MURRILL RJ; YEAGER WT JR et al.1981; J. AM. HELICOPTER SOC.; ISSN 0002-8711; USA; DA. 1981; VOL. 26; NO 2; PP. 31-39; BIBL. 4 REF.Article

AEROELASTIC BUFFETING PREDICTION TECHNIQUES. A GENERAL REVIEWFOERSCHING H.1981; FORSCHUNGSBER.-DTSCH. FORSCH.-VERSUCHSANST. LUFT-RAUMFAHRT; ISSN 0171-1342; DEU; DA. 1981; NO 15; PP. 1-53; ABS. GER; BIBL. 23 REF.Serial Issue

ETUDE DE SECURITE SUR DES PLANEURS ULTRA-LEGERS DE FORMULE ROGALLO. AERODYNAMIQUE ET MECANIQUE DU VOLLA BURTHE C; WALDEN S.1979; OFF. NATION. ET. RECH. AEROSPAT., NOTE TECH.; FRA; DA. 1979; NO 8; 226 P.; ABS. ENG; BIBL. 19 REF.Serial Issue

AEROELASTIC STABILITY ANALYSIS OF SUPERSONIC CASCADESSTRADA JA; CHADWICK WR; PLATZER MF et al.1979; J. ENG. POWER; ISSN 0022-0825; USA; DA. 1979; VOL. 101; NO 4; PP. 533-541; BIBL. 28 REF.Article

AEROELASTICITY RESEARCH FOR TURBOMACHINE APPLICATIONSFLEETER S.1979; J. AIRCR.; USA; DA. 1979; VOL. 16; NO 5; PP. 320-326; BIBL. 36 REF.Article

INSTRUMENTAL VARIABLES ALGORITHM FOR MODAL PARAMETER IDENTIFICATION IN FLUTTER TESTINGJOHNSON W; GUPTA NK.1978; A.I.A.A. J., NEW YORK; USA; DA. 1978; VOL. 16; NO 8; PP. 800-806; BIBL. 12 REF.Article

INFLUENCE OF MODELING AND BLADE PARAMETERS ON THE AEROELASTIC STABILITY OF A CANTILEVERED ROTOR.FRIEDMAN P.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 2; PP. 149-158; BIBL. 12 REF.Article

SOME SUGGESTIONS CONCERNING LINEAR THEORY OF AERO- AND HYDRO-ELASTICITY.BISHOP RED; BURCHER RK; PRICE WG et al.1976; STROJN. CAS.; CESKOSL.; DA. 1976; VOL. 27; NO 1-2; PP. 14-22; ABS. SLOVAQUE; BIBL. 9 REF.Article

TURBULENCE, BLUFF BODY AERODYNAMICS AND WIND ENGINEERINGMELBOURNE WH.sdAUSTRALASIAN CONFERENCE ON HYDRAULICS AND FLUID. 7/1980/BRISBANE; AUS; BARTON: INSTITUTION OF ENGINEERS, AUSTRALIA; DA. S.D.; PP. 9-14; BIBL. 15 REF.Conference Paper

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