Tank Tests of Auxiliary Vanes as a Substitute for Planing Area (1934)
NASA Technical Reports Server (NTRS) · leaf 10
N.A.C.A. Teohnical Note No. 490 Fig. 3 Figure 3.- Curves of resistance, A/r, rise of center of gravity, trim angle, and trimming moment fo Model 9. Model initial load, 112 lb. Model get-away speed, 39.4 feet per second.
NASA Technical Reports Server (NTRS)
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