Investigation made for thin flat plate wings for steady vertical and longitudinal motions, steady rolling and pitching and motions in which wing is accelerating uniformly in vertical direction.
Theoretical relations between stability derivatives of wing in direct and in reverse supersonic flow
Nat Advisory Committee Aeronautics -- Tech Note
1949
47 pages
Diagrs
Report
English
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Summary of lateral-stability derivatives calculated for wing plan forms in supersonic flow
Engineering Index Backfile | 1951
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