MCQs
Total Questions : 104
| Page 9 of 11 pages
Answer: Option A. -> 1430 to 1440
-NA-
Answer: Option C. -> Artificial Horizon
-NA-
Answer: Option D. -> Sweep back, dihedral and high wing
-NA-
Answer: Option A. -> continuous but not differentiable
-NA-
Question 85. A wing-body alone configuration airplane with a wing loading of W/S = 1000 N/m2 is flying in cruise condition at a speed V = 90m/s at sea-level (air density at sea-level P∞ = 1.22 kg/m3). The zero lift pitching moment coefficient of the airplane is Cwbmac = Cm0 = -0.06 and the location of airplane aerodynamic center from the wing leading edge is Xac = 0.25c. Here c is the chord length. Distance of center of gravity of the aircraft (XCG) from the wing leading edge is
Answer: Option C. -> 0.547c
-NA-
Answer: Option D. -> IV
-NA-
Answer: Option C. -> he displayed modesty in his interactions.
-NA-
Answer: Option B. -> 3/11 ≤ X/Y ≤ 5/8
-NA-
Answer: Option C. -> want
-NA-
Answer: Option B. -> electricity: wire
-NA-