Use the method of successive approximation (at least 3 approximations) to compute for the lift, drag, tail load and forward inertia force for the aircraft having the following specifications: Aircraft Model/Make: Cessna 172 Skyhawk Category: Normal MTOW: 2558 b Cruise speed: 124 knots wing area: 174 ft² Load Factor in: 1₁ Distance from the center of pressure of the tail plane to aircraft CG: 15'2" Assume engine-off conditions Use the curves for the angle of attack, drag coefficient and moment coefficient as shown below.

Use the method of successive approximation (at least 3 approximations) to compute for the lift, drag, tail load and forward inertia force for the aircraft having the following specifications: Aircraft Model/Make: Cessna 172 Skyhawk Category: Normal MTOW: 2558 b Cruise speed: 124 knots wing area: 174 ft² Load Factor in: 1₁ Distance from the center of pressure of the tail plane to aircraft CG: 15'2" Assume engine-off conditions Use the curves for the angle of attack, drag coefficient and moment coefficient as shown below.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Question

Use the method of successive approximation (at least 3 approximations) to compute for the lift, drag,
tail load and forward inertia force for the aircraft having the following specifications:
Aircraft Model/Make: Cessna 172 Skyhawk
Category:
Normal
MTOW: 2558 lb
Cruise speed: 124 knots
wing area: 174 ft²
Load Factor in: 1₂
Distance from the center of pressure of the tail plane to aircraft CG: 15'2"
Assume engine-off conditions
Use the curves for the angle of attack, drag coefficient and moment coefficient as shown below.
Co a m.cat
0.20 20 0.10
0.15 15 0.075
0.10 10 0.05
0.05 5 0.025
0 0
0.5
Cu,C6
1.0
(a)
Co
1.5
+G₂

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