kw.\*:("AEROELASTIC FLUTTER")
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GEARED-ELEVATOR FLUTTER STUDY.RUHLIN CL; DOGGETT RV JR; GREGORY RA et al.1976; IN: STRUCT. STRUCT. DYN. MATER. CONF. 17. PROC.; KING OF PRUSSIA, PA.; 1976; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; PP. 598-607; BIBL. 5 REF.Conference Paper
TEST OF PINES APPROXIMATE METHOD IN A FLUTTER CALCULATION FOR THE VIGGEN AIRCRAFT.STARK VJE.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 7; PP. 702-703; BIBL. 5 REF.Article
COMPARISON OF SUPERCRITICAL AND CONVENTIONAL WING FLUTTER CHARACTERISTICS.FARMER MG; HANSON PW.1976; IN: STRUCT. STRUCT. DYN. MATER. CONF. 17. PROC.; KING OF PRUSSIA, PA.; 1976; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; PP. 608-614; BIBL. 4 REF.Conference Paper
FLUTTER AND GUST RESPONSE ANALYSIS OF FLEXIBLE AIRCRAFT WITH ACTIVE CONTROL.NOLL RB; MORINO L.1976; IN: STRUCT. STRUCT. DYN. MATER. CONF. 17. PROC.; KING OF PRUSSIA, PA.; 1976; S.L.; AM. INST. AERONAUT. ASTRONAUT.; DA. 1976; PP. 389-397; BIBL. 14 REF.Conference Paper
A PRACTICAL OPTIMUM SELECTION PROCEDURE FOR A MOTIVATOR IN ACTIVE FLUTTER SUPPRESSION SYSTEM DESIGN ON AN AIRCRAFT WITH UNDERWING STORES.TURNER MR; LODGE CG.1977; A.G.A.R.D. CONF. PROC.; FR.; DA. 1977; NO 228; PP. 1-9Article
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
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
EINFLUSS SCHRAEGER HINTERKRANTEN UND EINFLUSS DES EIGENGEWICHTS DER BESPANNUNG AUF DIE UMSTROEMUNG KONISCHER PARAGLEITER MIT SCHWACHER WOELBUNG IM UEBERSCHALL. = INFLUENCE DES BORDS DE FUITE OBLIQUES ET DU POIDS DU REVETEMENT SUR L'ECOULEMENT AUTOUR DES PARAPLANEURS A FAIBLE COURBURE CONIQUE EN SUPERSONIQUEWAGNER B.1976; Z. FLUGWISSENSCH.; DTSCH.; DA. 1976; VOL. 24; NO 6; PP. 329-340; ABS. ANGL. FR.; BIBL. 8 REF.Article
APPLICATION OF A RAND-DEVELOPED NON LINEAR PROGRAMMING METHOD TO FLUTTER OPTIMIZATION.PHOA YT; CHI FH.1976; COMPUTERS AND STRUCT.; G.B.; DA. 1976; VOL. 6; NO 4-5; PP. 305-312; BIBL. 3 REF.Article
CONTINUATION AND DIRECT SOLUTION OF THE FLUTTER EQUATION.CARDANI PAOLO MANTEGAZZA C.1978; COMPUTERS AND STRUCT.; G.B.; DA. 1978; VOL. 8; NO 2; PP. 185-192; BIBL. 17 REF.Article
PIPES SUPPORTED AT BOTH ENDS CANNOT FLUTTERHOLMES PJ.1978; J. APPL. MECH.; USA; DA. 1978; VOL. 45; NO 3; PP. 619-622; BIBL. 12 REF.Article
SELF-EXCITED AEROELASTIC INSTABILITY OF A BRIDGE DECK.BELIVEAU JG.1977; J. FLUIDS ENGNG; U.S.A.; DA. 1977; VOL. 99; NO 3; PP. 452-456; BIBL. 10 REF.Article
FLUTTER OF ASYMMETRICALLY SWEPT WINGS.WEISSHAAR TA; CRITTENDEN JB.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 8; PP. 993-994; BIBL. 5 REF.Article
FLUTTER OF THERMALLY BUCKLED FINITE ELEMENT PANELS.YANG TY; HAN AD.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 7; PP. 975-977; BIBL. 9 REF.Article
UNIFIED PANEL FLUTTER THEORY WITH VISCOUS DAMPING EFFECTSOYIBO GA.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 5; PP. 767-773; BIBL. 24 REF.Article
NONLINEAR TRANSONIC FLUTTER ANALYSISBORLAND CJ; RIZZETTA DR.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 11; PP. 1606-1615; BIBL. 41 REF.Article
ON THE ROLE OF SHOCKS IN THE "SUB-TRANSONIC" FLUTTER PHENOMENONASHLEY H.1979; STRUCTURES, STRUCTURAL DYNAMICS, AND MATERIALS CONFERENCE. 20/1979/ST LOUIS MO; USA; DA. 1979; VOL. 2; PP. 162-177; BIBL. 34 REF.Conference Paper
A FLUTTER ANALYSIS OF A SYSTEM OF TWO AIRFOILS WITH AERODYNAMIC INTERFERENCE.GRZEDZINSKI J.1978; ARCH. MECH.; POLAND; DA. 1978; VOL. 30; NO 1; PP. 47-64; ABS. POL. RUSSE; BIBL. 9 REF.Article
UNSTEADY FLOW IN A SUPERSONIC CASCADE WITH STRONG IN-PASSAGE SHOCKS.GOLDSTEIN ME; BRAUN W; ADAMCZYK JJ et al.1977; J. FLUID MECH.; G.B.; DA. 1977; VOL. 83; NO 3; PP. 569-604; BIBL. 1 P.Article
EFFECT OF PHASE ANGLE ON MULTIBLADED ROTOR FLUTTER.MURTHY VR; PIERCE GA.1976; J. SOUND VIBR.; G.B.; DA. 1976; VOL. 48; NO 2; PP. 221-234; BIBL. 14 REF.Article
TRANSONIC BLADE FLUTTER: A SURVEY OF NEW DEVELOPMENTSPLATZER MF.1982; SHOCK VIB. DIG.; ISSN 0583-1024; USA; DA. 1982; VOL. 14; NO 7; PP. 3-8; BIBL. 30 REF.Article
DETERMINATION ET MAXIMISATION DE LA CHARGE CRITIQUE D'UNE COLONNE DE HAUGER EN PRESENCE D'AMORTISSEMENT.CLAUDON JL.1978; Z. ANGEW. MATH. PHYS.; SCHWEIZ; DA. 1978; VOL. 29; NO 2; PP. 226-236; ABS. ANGL.; BIBL. 20 REF.Article
FLUTTER OF AN ELASTIC PLATE UNDER TENSION.DOWELL EH; VENTRES CS.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 11; PP. 1653-1655; BIBL. 9 REF.Article
ON WAKE-INDUCED FLUTTER OF A CIRCULAR CYLINDER IN THE WAKE OF ANOTHER.TSUI YT.1977; J. APPL. MECH.; U.S.A.; DA. 1977; VOL. 44; NO 2; PP. 194-200; BIBL. 34 REF.Article
DRAG EFFECTS ON WING FLUTTER.PETRE A; ASHLEY H.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 10; PP. 755-763; BIBL. 7 REF.Article