Material given completes presentation indexed in Engineering Index 1953 p 56 from Tech Notes 2831 and 2898.
Theoretical calculations of effects of finite sideslip at supersonic speeds on span loading and rolling moment for families of thin sweepback tapered wings at angle of attack
NACA -- Tech Note
1953
53 pages
Report
English
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Rolling and yawing moments for swept-back wings in sideslip at supersonic speeds
Engineering Index Backfile | 1951
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