Publication Date:
2019-07-13
Description:
Flexible rotor blade dynamic response to radially moving force, emphasizing helicopter rotor vibration characteristics associated with tip- vortex impingement
Keywords:
AIRCRAFT
Type:
AIAA PAPER 69-203
,
VTOL RESEARCH, DESIGN, AND OPERATIONS MEETING; Feb 17, 1969 - Feb 19, 1969; ATLANTA, GA
Format:
text
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