Art

J-GLOBAL ID：200902195647857385   Reference number：01A0585084

Aeroelastic Divergence and Lateral Buckling of Free-Fixed Elastic Strip in Uniform Flow.

一様流中の自由-固定弾性片の静的空力発散と横挫屈

Author (1)： YAMAMOTO YUZO (岐阜工高専)
Material： 日本航空宇宙学会論文集  (Journal of the Japan Society for Aeronautical and Space Sciences)
Volume： 49  Issue： 568  Page： 135-140  Publication year： May. 05, 2001 
JST Material Number： L3565A  ISSN： 1344-6460  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： JAPANESE (JA)

Thesaurus term： *wing loading ,...
Semi thesaurus term： slender wing

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JST classification (1)： Aerodynamics of aircrafts  (QK02010T)

Reference (21)：

• 1) Yamamoto, Y.: Aeroelastic Divergence of Front-Free-Aft-Fixed Elastic Strip Parallel to Uniform Flow, Trans. Jpn. Soc. Aero. Space Sci., 31 (1989), pp. 188-194.
• 2) Jones, R.T.: Properties of Low-Aspect-Ratio Pointed Wings at Speeds below and above the Speed of Sound, NACA Rep. 835, 1946, pp. 59-63.
• 3) Miles, J.W.: Slender Body Theory for Supersonic Unsteady Flow, J. Aeronaut. Sci., 19 (1952), pp. 280-281.
• 4) Lamer, J.E. and Gloss, B.B.: Subsonic Aerodynamic Characteristics of Interacting Lifting Surface with Separated Flow around Sharp Edges Predicted by a Vortex-Lattice Method, NASA TN D-7921, 1975, pp. 1-89.
• 5) Katz, J. and Plotkin, A.: Low-Speed Aerodynamics from Wing Theory to Panel Method, McGraw-Hill, New York, 1991.

Terms in the title (5)： 一様流 ,  弾性片 ,  空力 ,  発散 ,  挫屈