Which of the following is the correct formula of ground run distance with respect to aircraft weight?

Question

TuteeHUB · Accepted Answer

NA

TuteeHUB · Answer

SG=$\frac{WV_{LOF}^2}{2g[F_N+D+\mu (W-L)]_{0.7V_{LOF}^2}}$

TuteeHUB · Answer

SG=$\frac{WV_{LOF}^2}{2g[F_N-D+\mu (W-L)]_{0.7V_{LOF}^2}}$

TuteeHUB · Answer

SG=$\frac{WV_{LOF}^2}{2g[F_N+D-\mu (W-L)]_{0.7V_{LOF}^2}}$

TuteeHUB · Answer

SG=$\frac{WV_{LOF}^2}{2g[F_N-D-\mu (W-L)]_{0.7V_{LOF}^2}}$

1.	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=\(\frac{WV_{LOF}^2}{2g[F_N-D-\mu (W-L)]_{0.7V_{LOF}^2}}\)
Answer» E.

Discussion