You are given a set of aircraft data from the results of the preliminary design of a business jet (refer the Appendix).

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You Are Given A Set Of Aircraft Data From The Results Of The Preliminary Design Of A Business Jet Refer The Appendix 1 (33.71 KiB) Viewed 13 times

You are given a set of aircraft data from the results of the preliminary design of a business jet (refer the Appendix). Determine the longitudinal static stability of 0 Wing contribution # Tail contribution m) Fuselage contribution to the pitching moment. Describe and plot these contributions and analyze their effects to the whole airplane (ie, the total pitching moment). Lastly, you need to recommend the change of the design based on your results to make the airplane stable if necessary. Appendix Wing: b = 52ft S - 519.5ft* < = 8.92/ A = 25° Cm -0.04 -0.1057" a = -1 X = 0.25c -0.35c Tail: 11 = 20.2ft Se = 121ft by = 24.25ft A = 10 Ch 0.1/ Eg = 0 7-1 4-0 4-2° Fuselage: Station 1 2 3 4 5 6 7 8 9 10 Ax 2.6 2.6 2.2 2.2 3.4 3.4 3.4 3.4 14.6 5.2 w 2.5 42 5.5 6.3 6.6 7 7.2 7.2 7.2 6.6 21.9 19.3 16.9 14.7 11.9 8.5 3.7 0 2.7 -3 -10 -10 0 0 0 0 + D A. 1. NINO LO 11 5.2 5.4 7.9 12 13 5.2 5.2 3.8 2.1 13.1 18.3 0 -4 5.1 Ollyll wlo