Research Catalog

Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing

Title
Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing [microform] / Paul A. Mirick, M-Nabil H. Hamouda, William T. Yeager.
Author
Mirick, Paul A.
Publication
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.

Details

Additional Authors
  • Hamouda, M-Nabil H.
  • Yeager, William T.
  • United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Description
1 v.
Series Statement
NASA technical memorandum ; 4224
Alternative Title
Wind tunnel survey of an oscillating flow field for applciation to model helicopter rotor testing
Subject
  • Aeroelasticity
  • Flow distribution
  • Gust loads
  • Helicopter performance
  • Oscillating flow
  • Wind tunnel tests
Note
  • Distributed to depository libraries in microfiche.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:4224
OCLC
marcive32399844
Author
Mirick, Paul A.
Title
Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing [microform] / Paul A. Mirick, M-Nabil H. Hamouda, William T. Yeager.
Imprint
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990.
Series
NASA technical memorandum ; 4224
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.
Added Author
Hamouda, M-Nabil H.
Yeager, William T.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:4224
Research Call Number
READEX Microfiche NAS 1.15:4224
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