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The 200-kg glider B is being towed by airplane A, which is flying horizontally with a constant speed of v = 194 km/h. The tow cable has a length r= 59 m and may be assumed to form a straight line. The glider is gaining altitude and when e reaches 16°, the angle is increasing at the constant rate = 3 deg/s. At the same time the tension in the tow cable is 1550 N for this position. Calculate the aerodynamic lift L and drag D acting on the glider. Assume o = 12°. B A

The 200-kg glider B is being towed by airplane A, which is flying horizontally with a constant speed of v = 194 km/h. The tow cable has a length r= 59 m and may be assumed to form a straight line. The glider is gaining altitude and when e reaches 16°, the angle is increasing at the constant rate = 3 deg/s. At the same time the tension in the tow cable is 1550 N for this position. Calculate the aerodynamic lift L and drag D acting on the glider. Assume o = 12°. B A

Structural Analysis
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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The 200-kg glider Bis being towed by airplane A, which is flying horizontally with a constant speed of v = 194 km/h. The tow cable has a length r = 59 m and may be assumed to form a straight line. The glider is gaining altitude and when ereaches 16, the angle is increasing at the constant rate 0 = 3 deg/s. At the same time the tension in the tow cable is 1550 N for this position. Calculate the aerodynamic lift L and drag D acting on the glider. Assume o = 12°. D B A
Transcribed Image Text:The 200-kg glider Bis being towed by airplane A, which is flying horizontally with a constant speed of v = 194 km/h. The tow cable has a length r = 59 m and may be assumed to form a straight line. The glider is gaining altitude and when ereaches 16, the angle is increasing at the constant rate 0 = 3 deg/s. At the same time the tension in the tow cable is 1550 N for this position. Calculate the aerodynamic lift L and drag D acting on the glider. Assume o = 12°. D B A
Calculate the aerodynamic lift Land drag D acting on the glider. Answers: L = i D =
Transcribed Image Text:Calculate the aerodynamic lift Land drag D acting on the glider. Answers: L = i D =
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