Question

rplane for which the starboard half-wing has the geometry give in Figure 1. For this wing, the lift curve slope is CLaw 5.0 per radian and the aileron flap effectiveness parameter is 0.2 Estimate the aileron power Cl for the airplane. (This and the next problem refer back to the Topic 3 notes. You might also inthe supplemenial ro Aerodynamic Properties relevant.) 2.75 m I Cfc-0.25 1.34 m 3.4 m 4.8 m 5.2m Figure 1: Half-wing of an airplane for Problems 3 and 4

Answer 1

み7S 1-gy うc The chord of a ー0 じ. 2 1.441 1.S1 m S, V) m2 인 10 . 629m 2- ed with nner 0

2 t aileron fap effei tenes S: a1. 26 ㄐ CD q ): 2.TS_o. 3.1 1-8 0.136 ns) PLEASE OPVO1E) canned with Seanner 2