Static longitudinal stability of "Ente" airplanes (1931)
NASA Technical Reports Server (NTRS) · leaf 32
N..A,C,A, Technical Memorandum No•612 Figs.11a,lib,12 … Fig.12 For a given C.G, location and a the stability is proportional to the (^mHo^2 ^iiig^^ difference between -4^ (( ^Cmg /<ia>dcja /da).
NASA Technical Reports Server (NTRS)
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