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Approximation method for determining the static stability of a monoplane glider (1927)
NASA Technical Reports Server (NTRS) · leaf 19
N„A.C.A.. Technical Memorandum No.436 Figs.8,9. … Fig.8, 100cm 0 10 30 30 40 120 100 80 60 100c a 40 20 0 -20 -8 -6 -4 -2 0 2 4 6 8 Fig.9 398 Gottingen airfoil..NASA Technical Reports Server (NTRS)
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