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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

TEZISY DOKLADOV/8 VSESOYUZNAYA KONFERENTSIYA PO AEHROUPRUGOSTI TURBOMASHIN, KIEV, 28.9-1.10 1981 GODA = RESUMES DES COMMUNICATIONS/8EME CONFERENCE FEDERALE SUR L'AEROELASTICITE DES TURBOMACHINES, KIEV, 28.9-1.10 1981PISARENKO GS ED.1981; VSESOYUZNAYA KONFERENTSIYA PO AEHROUPRUGOSTI TURBOMASHIN. 8/1981-09-28/KIEV 1981; UKR; KIEV: NAUKOVA DUMKA; DA. 1981; 68 P.; 21 CMConference Proceedings

WING STORE ACTIVE FLUTTER SUPPRESSION: CORRELATION OF ANALYSES AND WINDTUNNEL DATANOLL TE; HUTTSELL LJ.1979; J. AIRCR.; USA; DA. 1979; VOL. 16; NO 7; PP. 491-497; BIBL. 8 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

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

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

Verification of H Flutter AnalysisHOUNJET, Michaël H. L.Journal of aircraft. 2010, Vol 47, Num 6, pp 2168-2174, issn 0021-8669, 7 p.Article

Unified aeroelastic flutter theory for very low aspect ratio panelsOYIBO, G. A.AIAA journal. 1983, Vol 21, Num 11, pp 1581-1587, issn 0001-1452Article

Unsteady and non-linear aeroelastic analysis of large horizontal-axis wind turbinesMAZA, Mauro S; PREIDIKMAN, Sergio; FLORES, Fernando G et al.International journal of hydrogen energy. 2014, Vol 39, Num 16, pp 8813-8820, issn 0360-3199, 8 p.Conference Paper

PROBLEMES DE L'AEROHYDROELASTICITE DES CORPS A CONTRAINTES INITIALESGUZ AN.1980; PRIKL. MEKH.; UKR; DA. 1980; VOL. 16; NO 3; PP. 3-21; BIBL. 28 REF.Article

ESTIMATION OF STRUCTURAL SYSTEM PARAMETERS FROM STATIONARY AND NON-STATIONARY AMBIENT VIBRATIONS: AN EXPLORATORY-CONFIRMATORY ANALYSISGERSCH W; MARTINELLI F.1979; J. SOUND VIBR.; GBR; DA. 1979; VOL. 65; NO 3; PP. 303-318; BIBL. 24 REF.Article

FORMULATION OF THE AEROELASTIC STABILITY AND RESPONSE PROBLEM OF COUPLED ROTOR/SUPPORT SYSTEMSWARMBRODT W; FRIEDMANN P.1979; STRUCTURES, STRUCTURAL DYNAMICS, AND MATERIALS CONFERENCE. 20/1979/ST LOUIS MO; USA; DA. 1979; VOL. 2; PP. 39-52; BIBL. 23 REF.Conference Paper

HYPERSONIC AEROTHERMOELASTIC CHARACTERISTICS OF A FINNED MISSILEERICSSON LE; ALMROTH BO; BAILIE JA et al.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-231; 8 P.; BIBL. 29 REF.Conference Paper

ON THE OPTIMIZATION OF DISCRETE STRUCTURES WITH AEROELASTIC CONSTRAINTS.MCINTOSH SC JR.1978; COMPUTERS AND STRUCT.; G.B.; DA. 1978; VOL. 8; NO 3-4; PP. 411-419; BIBL. 22 REF.Article

WINDFORCES ON AN EXCITATION OF A 130-M CONCRETE CHIMNEY.CHRISTENSEN O.1978; J. INDUSTR. AERODYN.; NETHERL.; DA. 1978; VOL. 3; NO 1; PP. 61-77; BIBL. 8 REF.Article

STABILITY DERIVATIVE MEASUREMENTS WITH MAGNETICALLY SUSPENDED CONE-CYLINDER MODELS.BHARATHAN D; FISHER SS.1977; J. SPACECR. ROCK.; U.S.A.; DA. 1977; VOL. 14; NO 12; PP. 719-723; BIBL. 13 REF.Article

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

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

SYSTEME D'EXCITATION POUR ESSAIS INSTATIONNAIRES EN SOUFFLERIE SUR DEMI-MAQUETTE DE VOILUREDESTUYNDER R.1983; RECHERCHE AEROSPATIALE; ISSN 0034-1223; FRA; DA. 1983; NO 3; PP. 215-216Article

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