Title: Oscillating rectangular wings in supersonic flow with arbitrary bending and torsion mode shapes. Part II: Numerical results
Abstract: As has been shown in part I the aerodynamic derivatives can be given in the form of the sum of some terms each of which consists of two factors, one being a function of the reduced frequency and the Mach number, the other one containing the bending or the torsion mode shape. Tables of the factors containing the reduced frequency k and the Mach number M are presented for k=0 (0.1) 1 and M = 1.2 (0.1) 1.6 (0.2) 2 (0.5) 4. In order to show the influence of frequency. Mach number and aspect ratio graphs are given of the aerodynamic derivates for a translating and pitching flat wing. They have been plotted as functions of the reduced frequency for different values of aspect ratio and Mach number.
Publication Year: 1959
Publication Date: 1959-12-31
Language: en
Type: article
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