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Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions

Author(s):
Publication title:
NASA Technical Reports
Pub. Year:
1995
Issue:
NASA-CR-198590
Pt.:
NAS 1.26:198590
Paper no.:
N95-28193
Page(from):
1
Page(to):
53
Pages:
53
Pub. info.:
National Aeronautics and Space Adminstration
Language:
English
Type:
Technical Paper

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