Available results summarized; effects of aspect ratio and Mach number studied, and subsonic values for derivatives included in investigation of Mach number effects; non-linearities in sideslip variation of yawing and rolling moments; effects of combining wing and body indicated for two of derivatives.
Theoretical lateral-stability derivatives for wings at supersonic speeds
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 17 , n 1
1950
Bibliography
Article (Journal)
English
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Stability derivatives of triangular wings at supersonic speeds
TIBKAT | 1948
|Stability derivatives of triangular wings at supersonic speeds
Engineering Index Backfile | 1948
|Stability derivatives of triangular wings at supersonic speeds
Engineering Index Backfile | 1948
|