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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

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

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

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

UNRESTRAINED AEROELASTIC DIVERGENCE IN A DYNAMIC STABILITY ANALYSISRODDEN WP; BELLINGER ED.1982; J. AIRC.; ISSN 0021-8669; USA; DA. 1982; VOL. 19; NO 9; PP. 796-797; BIBL. 14 REF.Article

VIBRATIONS OF A COMPRESSOR BLADE WITH SLIP AT THE ROOTJONES DIG; MUSZYNSKA A.1978; SHOCK VIBR. BULL.; USA; DA. 1978; NO 48 PART. 2; PP. 53-61; BIBL. 13 REF.Article

ETUDE DE LA RELATION ENTRE L'AMPLITUDE ET L'AMORTISSEMENT A L'AIR DES AILETTES D'UNE TURBINE.AVDEEV VB.1978; PROBL. MASHINOSTR.; UKR; DA. 1978; NO 6; PP. 56-60; BIBL. 3 REF.Article

MODEL TESTS ON FLOW-INDUCED VIBRATIONS OF BRIDGE DECKS OF THE CHANNEL TYPE.HJORTH HANSEN E.1977; J. INDUSTR. AERODYN.; NETHERL.; DA. 1977; VOL. 2; NO 2; PP. 113-128; BIBL. 7 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

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