Flow structure generated by perpendicular blade-vortex interaction and implications for helicopter noise prediction.

Flow structure generated by perpendicular blade-vortex interaction and implications for helicopter noise prediction.

Author(s):

Wittmer, Kenneth S. ( Virginia Polytechnic Institute and State University )
Devenport, William J.

Publication title:

NASA Technical Reports

Pub. Year:

1996

Vol.:

19960014827

Issue:

NASA-CR-200159

Pt.:

NAS 1.26:200159

Paper no.:

N96-21271

Page(from):

1

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001432

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