Formulas for supersonic loading, lift, and drag of flat swept-back wings with leading edges behind mach lines. (35¢)
Formulas for supersonic loading, lift, and drag of flat swept-back wings with leading edges behind mach lines
NACA -- Report
1951
40 pages
Diagrams, Charts
Report
Englisch
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Engineering Index Backfile | 1947
|Theoretical lift of flat swept-back wings at supersonic speeds
Engineering Index Backfile | 1948
|