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
English
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Engineering Index Backfile | 1949
|Theoretical relations between stability derivatives of wing in direct and in reverse supersonic flow
Engineering Index Backfile | 1949
|