Results of landing tests of various airplanes
Description:
Report presenting a study of the landing characteristics of various airplanes with special attention paid to problems with landing gear design. The planes ranged from 1000 to 50,000 pounds and in span from 28 to 149 feet. Results regarding the observed landing conditions, including attitude, vertical velocity, pitching velocity, rolling velocity, lateral velocity (or side drift), and landing gear loads measured during the tests are provided.
Date:
September 1942
Creator:
Hootman, J. A. & Jones, A. R.
Item Type:
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