Influence of Cut-outs in Elevator on the Static Longitudinal Stability and on the Static Elevator Effect (1934)
NASA Technical Reports Server (NTRS) · leaf 5
Figs. 1,2,3,4 N.A, C.A, Technical Memorandum No. 750 … N = 90 hp. Etogine performance ? = 14.7 m2 Wing area 11.3 m Wing span 1.34m Mean chord 380 kg Net weight Full load (depending on e.g. position) 5? = 529 to 571 kg Figure 1.- Airplane with modified tail surface. Figure 2.- Outline of original and modified elevator.
NASA Technical Reports Server (NTRS)
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