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Which of the following is the correct formula of ground run distance with respect to aircraft weight?(a) SG=\(\frac{WV_{LOF}^2}{2g[F_N+D+\mu (W-L)]_{0.7V_{LOF}^2}}\)(b) SG=\(\frac{WV_{LOF}^2}{2g[F_N-D+\mu (W-L)]_{0.7V_{LOF}^2}}\)(c) SG=\(\frac{WV_{LOF}^2}{2g[F_N+D-\mu (W-L)]_{0.7V_{LOF}^2}}\)(d) SG=\(\frac{WV_{LOF}^2}{2g[F_N-D-\mu (W-L)]_{0.7V_{LOF}^2}}\)This question was posed to me in class test.The doubt is from Effect on the Take-off Distances of Flight Variables topic in section Take-off and Landing Performance of Aircraft Performance |
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Answer» The correct option is (d) SG=\(\frac{WV_{LOF}^2}{2g[F_N-D-\mu (W-L)]_{0.7V_{LOF}^2}}\) |
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