Pls help! For a given wing-body combination, the aerodynamic center lies 0.03 chord lengthahead of the center of gravity. The moment coefficient about the center of gravity is0.005, and the lift coefficient is 0.5. Calculate the moment coefficient about theaerodynamic center. Geometric Data:Wing area, S = 1.5 ft² (0.139 m²), Wing mean aerodynamic chord, ☎ = 6.145 in (15.61 cm)1,= 15.29 in (38.84 cm),Tail area, S,= 0.368 ft² (0.0342 m²)Aerodynamic Data: Awb = 0.077/deg., at=0.064/deg., &o = 0.72 º20.018, h=0.25, p = 2.377x10-³ slugs/ft³ (1.225 kg/m³)deθα=0.3, C,macwb=

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For a given wing-body combination, the aerodynamic center lies 0.03 chord length ahead of the center of gravity. The moment coefficient about the center of gravity is 0.005, and the lift coefficient is 0.5. Calculate the moment coefficient about the aerodynamic center.

For a given wing-body combination, the aerodynamic center lies 0.03 chord length ahead of the center of gravity. The moment coefficient about the center of gravity is 0.005, and the lift coefficient is 0.5. Calculate the moment coefficient about the aerodynamic center.

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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Question

Pls help!

For a given wing-body combination, the aerodynamic center lies 0.03 chord length
ahead of the center of gravity. The moment coefficient about the center of gravity is
0.005, and the lift coefficient is 0.5. Calculate the moment coefficient about the
aerodynamic center.

Geometric Data:
Wing area, S = 1.5 ft² (0.139 m²), Wing mean aerodynamic chord, ☎ = 6.145 in (15.61 cm)
1,= 15.29 in (38.84 cm),Tail area, S,= 0.368 ft² (0.0342 m²)
Aerodynamic Data: Awb = 0.077/deg., at=0.064/deg., &o = 0.72 º
2
0.018, h=0.25, p = 2.377x10-³ slugs/ft³ (1.225 kg/m³)
de
θα
=
0.3, C,
macwb
=

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