Pascal and Francis Bibliographic Databases

Help

Search results

Your search

kw.\*:("Aeroelastic flutter")

Document Type [dt]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Publication Year[py]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Discipline (document) [di]

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Language

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Author Country

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Origin

A-Z Z-A Frequency ↓ Frequency ↑
Export in CSV

Results 1 to 25 of 919

  • Page / 37
Export

Selection :

  • and

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

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

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

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

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

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

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

ACTIVE FLUTTER SUPPRESSION ON AN AIRPLANE WITH WING MOUNTED EXTERNAL STORES.HONLINGER H.1977; A.G.A.R.D. CONF. PROC.; FR.; DA. 1977; NO 228; PP. 1-15; BIBL. 17 REF.Article

SOME RECENT DEVELOPMENTS IN UNSTEADY AERODYNAMICS OF A SUPERSONIC CASCADE.KUROSAKA M; EDELFELT IH.1976; R.F.M.; FR.; DA. 1976; NO. SPEC.; PP. 57-64; BIBL. 13 REF.; (AEROELASTICITE TURBOMACH. SYMP. IUTAM-ATTAG; PARIS; 1976)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

Flutter supression using linear optimal and fuzzy logic techniquesADIN, Zvi; BEN-ASHER, Joseph Z; COHEN, Kelly et al.Journal of guidance, control, and dynamics. 2003, Vol 26, Num 1, pp 173-177, issn 0731-5090, 5 p.Article

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

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

Wind-excited behaviour of structures IV = Comportement de structures excitées par le ventJOHNS, D. J.The Shock and vibration digest. 1985, Vol 17, Num 7, pp 17-34, issn 0583-1024Article

Berechnung subkritischer Eigenfrequenzen und Dämpfungen bei einer Flatteruntersuchung = Calcul des fréquences propres souscritiques et des amortissements dans une étude de flottement aéroélastique = Calculation of subcritical natural frequencies and damping rates in a flutter investigationWITTMEYER, H.Zeitschrift für Flugwissenschaften und Weltraumforschung. 1983, Vol 7, Num 5, pp 331-334, issn 0342-068XArticle

Transonic flutter model study of a supercritical wing and wingletRUHLIN, C. L; RAUCH, F. J. JR; WATERS, C et al.Journal of aircraft. 1983, Vol 20, Num 8, pp 711-716, issn 0021-8669Article

  • Page / 37