Given a radar dome of 300 lbm on the bottom of a surveillance aircraft attached by 4 bolts loaded in shear. The bolts each have an ultimate shear strength of 11,000 lbf. The airplane pulls up from a dive at 350KTAS. At the bottom of the pull-up the flight path radius is 6000 ft and there is 2000 Ibf drag and 1000 lb suction (negative lift) on the radome. At that point, determine the: a. Load factor b. Limit load per bolt c. Ultimate load per bolt d. Margin of Safety

Given a radar dome of 300 lbm on the bottom of a surveillance aircraft attached by 4 bolts loaded in shear. The bolts each have an ultimate shear strength of 11,000 lbf. The airplane pulls up from a dive at 350KTAS. At the bottom of the pull-up the flight path radius is 6000 ft and there is 2000 Ibf drag and 1000 lb suction (negative lift) on the radome. At that point, determine the: a. Load factor b. Limit load per bolt c. Ultimate load per bolt d. Margin of Safety

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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Given a radar dome of 300 lbm on the bottom of a surveillance aircraft attached by 4 bolts loaded in
shear. The bolts each have an ultimate shear strength of 11,000 lbf. The airplane pulls up from a
dive at 350KTAS. At the bottom of the pull-up the flight path radius is 6000 ft and there is 2000 Ibf
drag and 1000 lb suction (negative lift) on the radome. At that point, determine the:
a. Load factor
b. Limit load per bolt
c. Ultimate load per bolt
d. Margin of Safety

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