The aircraft velocity $(\mathrm{m} / \mathrm{s})$ components in body axes are given as $[u, v, w]=[100,10,10] .$ The air velocity $(\mathrm{m} / \mathrm{s})$, angle of attack (deg) and sideslip angle (deg) in that order are

(A) [120,0.1,0.1]

(B) [100,0.1,0.1]

(C) [100.995,0.1,5.73]

(D) [100.995,5.71,5.68]

The aircraft velocity $(\mathrm{m} / \mathrm{s})$ components in body axes are given as $[u, v, w]=[100,10,10] .$ The air velocity $(\mathrm{m} / \mathrm{s})$, angle of attack (deg) and sideslip angle (deg) in that order are

(A) [120,0.1,0.1]

(B) [100,0.1,0.1]

(C) [100.995,0.1,5.73]

(D) [100.995,5.71,5.68]

127