Effect of Mach and Reynolds Numbers on Maximum Lift Coefficient Obtainable in Gradual and Abrupt Stalls of Pursuit Airplane Equipped with Low-Drag Wing. (Originally issued as Memorandum Report A5G06)
Effect of Mach and Reynolds numbers on maximum lift coefficient obtainable in gradual and abrupt stalls of pursuit airplane equipped with low-drag wing
Advisory Committee Aeronautics -- Wartime Report
1947
12 pages
Supp plates
Report
Englisch
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