Values of derivatives, calculated using linearized theory for compressible flow, presented in form of design charts showing variations of derivatives with Mach number and aspect ratio for nine plan forms. (30¢)
Summary of lateral-stability derivatives calculated for wing plan forms in supersonic flow
NACA -- Report
1951
35 pages
Charts, Tables, Bibliography
Report
Englisch
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Engineering Index Backfile | 1949
|Theoretical lateral-stability derivatives for wings at supersonic speeds
Engineering Index Backfile | 1950
|