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Influence of design on cost of operating airplanes (1922)
NASA Technical Reports Server (NTRS) · leaf 17
a-J-^y load. x b-Safety factor 8 c-Safety factor 6 d-Safety factor 4 e-I7ings f-Pilot g-Front fuselage, etc. h-Rea^r fuselage and tail i~Landing gear 3-Tanks k-C-asoline and oil l~Engine, propeller, radiator and water Total weight in lbs. 8400 6300 4300 … "80 90 100 110 130 1 30 140 High speed at 5000 ft- in M.P.H. (Liberty engine, constant minimum speed, 57 M.P,H.; duration, 4 to.; wing loading 10 lb. per sq*ft,) Fig. 4 Variation of weight di-Kinion with speed- 430 HP. airplane. »NASA Technical Reports Server (NTRS)
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