Numerical procedure for calculation of aerodynamic forces at subsonic Mach numbers on oscillating wings with unswept trailing edges; this is extension of method suggested in Tech Note 41 (see Engineering Index 1959 p 24); numerical applications presented for 4 rectangular wings at Mach number M=0 and for one rectangular aspect ratio 2 wing at M=0.9; tabulated results given for high order modes and several reduced frequencies in both cases.
Aerodynamic forces on rectangular wings oscillating in subsonic flow
Svenska Aeroplan Aktiebolaget -- Tech Note
1960
29 pages
Report
English
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