Incorrectness of the k method for flutter calculationsPATIL, Mayuresh J; YURKOVICH, Rudolph N; HODGES, Dewey H et al.Journal of aircraft. 2004, Vol 41, Num 2, pp 402-405, issn 0021-8669, 4 p.Article

The synthesis of an active flutter suppression law based on an energy criterionKLEIN, A. K.Aeronautical quarterly. 1983, Vol 34, Num 4, pp 260-281, issn 0001-9259Article

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

DESIGN STUDY OF STRUCTURAL CONCEPTS FOR AN ARROW-WING SUPERSONIC-CRUISE AIRCRAFT.SAKATA IF; DAVIS GW; ROBINSON JC et al.1975; IN: AM. INST. AERONAUT. ASTRONAUT. AIRCR. SYST. TECHNOL. MEET.; LOS ANGELES; 1975; NEW YORK; A.I.A.A.; DA. 1975; VOL. 1037; PP. 1-12; BIBL. 3 REF.Conference Paper

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

SIMULATION AU SOL DU FLOTTEMENT POUR LES AVIONS DE GRAND ALLONGEMENT.PERUMAL RAJAGOPAL.1974; OFF. NATION. ET. RECH. AEROSPAT., NOTE TECH.; FR.; DA. 1974; NO 222; PP. 1-48; BIBL. 19 REF.Article

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

Extension of flutter prediction parameter for multimode flutter systemsBAE, Jae-Sung; KIM, Jong-Yun; LEE, In et al.Journal of aircraft. 2005, Vol 42, Num 1, pp 285-288, issn 0021-8669, 4 p.Article

Parametric trends in the flutter of advanced turbopropsCRAWLEY, E. F; DUCHARME, E. H.Journal of turbomachinery. 1990, Vol 112, Num 4, pp 741-750, issn 0889-504X, 10 p.Conference Paper

Influence des déformations statiques d'une voilure sur l'aérodynamique instationnaire = Influence of the static deformation of a wing in the unsteady aerodynamicsDESTUYNDER, R.AGARD conference proceedings. 1987, Num 403, pp 11.1-11.8, issn 0549-7191Conference Paper

APPLICATION OF TRANSONIC CODES TO FLUTTER ANALYSIS OF CONVENTIONAL AND SUPERCRITICAL AIRFOILSYANG TY; GURUSWAMY P; STRIZ AG et al.1982; J. AIRCR.; ISSN 0021-8669; USA; DA. 1982; VOL. 19; NO 3; PP. 211-220; BIBL. 2 P.Article

THE ROLE OF THE NAE 5 X 5 FOOT WIND TUNNEL IN THE DEVELOPMENT OF MODERN AIRFOIL SECTIONS.OHMAN LH.1976; CANAD. AERONAUT. SPACE J.; CANADA; DA. 1976; VOL. 22; NO 1; PP. 1-22; BIBL. 33 REF.Article

UNSTEADY FLOW.1976; IN: SYMP. TRANSSONICUM. 2. INT. UNION THEOR. APPL. MECH.; GOETTINGEN; 1975; BERLIN; SPRINGER; DA. 1976; PP. 1-108; BIBL. DISSEM.Conference Paper

VIBRATIONS DU TYPE "FLUTTER" QUASI LINEAIRES DE TORSION ET DE FLEXION D'UN PROFIL D'AILEVOZNYUK AV; KRAVCHENKO VP.1975; VYCHISLIT. PRIKL. MAT., U.S.S.R.; S.S.S.R.; DA. 1975; NO 27; PP. 113-120; ABS. ANGL.; BIBL. 4 REF.Article

SIMULATION DU FLOTTEMENT AU SOL POUR LES AVIONS DE GRAND ALLONGEMENT.RAJAGOPAL P.1974; AO-CNRS-11849; FR.; DA. 1974; PP. 1-90; ABS. ANGL.; BIBL. 2 P.; (THESE DOCT.-ING.; PARIS VI)Thesis

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

PANEL FLUTTER OPTIMIZATION - A REFINED FINITE ELEMENT APPROACH. = OPTIMISATION DU FLOTTEMENT DES PANNEAUX. METHODE AUX ELEMENTS FINIS PERFECTIONNEEWEISSHAAR TA.1976; INTERNATION. J. NUMER. METHODS ENGNG; G.B.; DA. 1976; VOL. 10; NO 1; PP. 77-91; BIBL. 20 REF.Article

COMPARISON OF TWO TYPES OF STRUCTURAL OPTIMIZATION PROCEDURES FOR FLUTTER REQUIREMENTS.HAFTKA RT; STARNES JH JR; BARTON FW et al.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 10; PP. 1333-1339; BIBL. 17 REF.Article

A PERTURBATION METHOD FOR TRANSONIC FLOWS ABOUT OSCILLATING AIRFOILS.TRACI RM; ALBANO ED; FARR JL JR et al.1975; IN: ANN. INST. AERONAUT. ASTRONAUT. 8TH FLUID PLASMA DYN. CONF.; HARTFORD, CONN.; 1975; NEW YORK; DA. 1975; VOL. 872; PP. 1-12; BIBL. 22 REF.Conference Paper

ON THE HYDRODYNAMIC FLUTTER ANOMALY.CRISP JDC; BERREEN TF.1974; IN: NOISE SHOCK VIB. CONF. PROC.; MELBOURNE; 1974; CLAYTON; NSV CONF. ORGAN. COMM.; DA. 1974; PP. 54-61; BIBL. 7 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

PANEL FLUTTER OPTIMIZATION BY GRADIENT PROJECTION.PIERSON BL.1975; INTERNATION. J. NUMER. METHODS ENGNG; G.B.; DA. 1975; VOL. 9; NO 2; PP. 271-296; BIBL. 1 P. 1/2Article

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