Results indicate that partial-power vertical descents and landing approaches produce rotor blade moments that are higher than moments encountered in any other flight condition investigated.
Flight investigation of effects of transition, landing approaches. Partial-power vertical descents, and droop-stop pounding on bending and torsional moments encountered by helicopter rotor blade
NASA -- Memo
NASA -- Memorandum ; n 5-7-59L
1959
38 pages
Report
Englisch
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Engineering Index Backfile | 1958
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