Results of extended tests of the Focke-Wulf F 19a "ente," a tail-first airplane (1933)
NASA Technical Reports Server (NTRS) · leaf 22
Figs. 5,6 N.A.C.A. Technical Memorandum lTo.721 … 40 50 80 70 80 90 100 110 1§0 Dynamic pressure, q kg/m - Figure 5.-Climbing speed with e.g. at-26.0,-27.7, and -29.65$ of the mean wing chord. The airplane weight differed in each test flight. She e.g. at -29.65$ of tm is outside the acceptance limits. m/sec. J 1 cu ia no 0 ■H ^> •H , rH -1 O 110…
NASA Technical Reports Server (NTRS)
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