Analysis of gust response of simplified model of airplane having degrees of freedom of vertical motion and wing twist; 2-dimensional, incompressible unsteady flow is assumed.
Effects of wing twist on response of airplane encountering sharp-edged gust
J. Aeronautical Sciences
Journal of the Aeronautical Sciences ; 20 , n 12
1953
Aufsatz (Zeitschrift)
Englisch
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Rotor Blade Motion in a Vertical Sharp-edged Gust
Emerald Group Publishing | 1954
|Rotor Blade Motion in a Vertical Sharp-Edged Gust
Emerald Group Publishing | 1954
|Rotor Blade Motion in a Vertical Sharp-edged Gust
Emerald Group Publishing | 1954
|