Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles.
Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles
NACA -- Report
1955
60 pages
Report
Englisch
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Stability derivatives of triangular wings at supersonic speeds
Engineering Index Backfile | 1948
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