Investigation of loads produced upon wings and tail plane of airplane when pulled out of dive to determine satisfactory means of preventing structural failure under extreme conditions; variations made in gear ratio between elevator and control stick, in total time to pull back, in maximum hand load, and in initial diving speed; danger of failure through rough handling only avoided by limiting control load transmitted to elevators.
Loads on the main planes and tail of an aeroplane when recovering from a dive
Aeronautical Research Committee -- Reports Memoranda
1928
24 pages
8 Figs.
Report
Englisch
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