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kw.\*:("FUSELAGE AVION")

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A MIXED OPTIMIZATION METHOD FOR AUTOMATED DESIGN OF FUSELAGE STRUCTURES = METHODE D'OPTIMISATION MIXTE POUR LE CALCUL AUTOMATISE DES STRUCTURES DE FUSELAGESOBIESZCZANSKI J; LOENDORF D.sdIN: AIAA/ASME/SAE 13TH STRUCT. STRUCT. DYN. MATER. CONF. SAN ANTONIO, TEX., 1972. III; NEW YORK; AIAA; DA. S.D.; PP. 1-17; BIBL. 16 REF.Conference Paper

Modified component mode synthesis for aircraft structuresROOZEN, N.B; VAN BERLO, A.O.H; DE KRAKER, A et al.European conference on structural dynamics, EUDODYN'90. 1991, pp 969-976, 8 p.Conference Paper

ANALYSIS OF SELF-EXCITED AND FORCED VIBRATIONS OF A RECTANGULAR PLATE ON MANY SUPPORTS IN SUPERSONIC FLOWWIELGUS A.1972; PROC. VIBR. PROBL.; POLAND; DA. 1972; VOL. 13; NO 4; PP. 377-396; ABS. POL. RUSSE; BIBL. 11 REF.Serial Issue

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