Experiments with a device for shortening the glide and landing run of an airplane (1924)
NASA Technical Reports Server (NTRS) · leaf 16
N.A-C.A, Technical Memoxandum No.273 Figs.2&o. Angle of attack 12° ^ increase of ^ decrease of drag coefficient. lift coefficient. a. 79 a. 24 b-79 lb. 79 lb.24 B ^ g'.29 Jg.97 3g.97r p g.29- h.83 ' ' h.25 L i.21 Zii .72 E D -> 3.25 ■J D-S7 E im98 111.36 Fig.2 Result of test, … Fig.3 Comparison of morxienta during landing r\an.
NASA Technical Reports Server (NTRS)
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