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

H Flutter Analysis : A Direct Harmonic Interpolation MethodHOUNJET, Michaël H. L.Journal of aircraft. 2009, Vol 46, Num 1, pp 348-352, issn 0021-8669, 5 p.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

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

A root locus-based flutter synthesis procedurePRABHAT HAJELA.Journal of aircraft. 1983, Vol 20, Num 12, pp 1021-1027, issn 0021-8669Article

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

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

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

A REVIEW OF SOME TILT-ROTOR AEROELASTIC RESEARCH AT NASA-LANGLEY.KVATERNIK RG.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 5; PP. 357-363; BIBL. 10 REF.Article

Discrete conservation and coupling strategies in nonlinear aeroelasticityMASSJUNG, Ralf.Computer methods in applied mechanics and engineering. 2006, Vol 196, Num 1-3, pp 91-102, issn 0045-7825, 12 p.Article

Upper-bound flutter speed estimation using the μ-k methodBORGLUND, Dan.Journal of aircraft. 2005, Vol 42, Num 2, pp 555-557, issn 0021-8669, 3 p.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

Etude des paramètres du mouvement spatial d'un corps solide libre dans une formulation non linéaireKRAVETS, V. V; KRYSHKO, E. P.Prikladnaâ mehanika (Kiev). 1984, Vol 20, Num 11, pp 122-125, issn 0032-8243Article

FLUTTER LOADS OF A TIMOSHENKO BEAM-COLUMN UNDER A FOLLOWER FORCE GOVERNED BY TWO VARIANTS OF EQUATIONS OF MOTIONKATSIKADELIS JT; KOUNADIS AN.1983; ACTA MECHANICA; ISSN 0001-5970; AUT; DA. 1983; VOL. 48; NO 3-4; PP. 209-217; BIBL. 17 REF.Article

OPTIMIZATION OF STRUCTURES SUBJECTED TO AEROELASTIC INSTABILITY PHENOMENASEYRANIAN AP.1982; ARCHIVES OF MECHANICS; ISSN 0373-2029; POL; DA. 1982; VOL. 34; NO 2; PP. 133-146; ABS. POL/RUS; BIBL. 24 REF.Article

EFFECTS OF ENVIRONMENT, DAMPING AND SHEAR DEFORMATIONS ON FLUTTER OF LAMINATED COMPOSITE PANELSCHATTERJEE SN; KULKARNI SV.1979; INTERNATION. J. SOLIDS STRUCT.; GBR; DA. 1979; VOL. 15; NO 6; PP. 479-491; BIBL. 34 REF.Article

FLUTTER AND BUCKLING OF GENERAL LAMINATED PLATES.SAWYER JW.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 4; PP. 387-393; BIBL. 14 REF.Article

An analytical procedure for asymmetric store flutterLIU, J. K.Aeronautical Journal. 1999, Vol 103, Num 1028, pp 455-456, issn 0001-9240Article

STABILITY OF A RECTANGULAR PLATE UNDER NONCONSERVATIVE AND CONSERVATIVE FORCESADALI S.1982; NRIMS TECH. REP., TWISK; ISSN 501689; ZAF; DA. 1982; NO 245; PP. 1-18; H.T. 6; BIBL. 32 REF.Serial Issue

SUPERSONIC FLUTTER OF HEATED CIRCULAR CYLINDRICAL SHELLS WITH TEMPERATURE-DEPENDENT MATERIAL PROPERTIES.OLSSON U.1978; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1978; VOL. 16; NO 4; PP. 360-362; BIBL. 8 REF.Article