PEARSON ETEXT ENGINEERING MECH & STATS
PEARSON ETEXT ENGINEERING MECH & STATS
15th Edition
ISBN: 9780137514724
Author: HIBBELER
Publisher: PEARSON
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The answers I got for A and B are correct. The following is the remaining answers I got which are all INCORRECT:         Part C- 39.8, Part D- 119.511 lb*in, Part E- 278.86 lb*in
For nos. 21-23, satisfy the conditions of the given problem below: As an airplane's brakes are applied, the nose wheel exerts two forces on the end of the landing gear as shown in the figure 1. Determine: 21. the force in the strut AB. * 1 point 30° 450 lb. 1350 lb O A. 215.3 lb B. 224.4 lb C. 233. 2 lb D. 234.3 lb 1 ft 2 ft
B2
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