Research Catalog

Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions semi-annual report to NASA Langley for worked performed under the grant

Title
Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions [microform] : semi-annual report to NASA Langley for worked performed under the grant / principal investigators: William J. Devenport, Stewart A.L. Glegg.
Author
Devenport, William J.
Publication
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors
  • Glegg, Stewart A. L.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA contractor report ; NASA CR-198590
Subject
  • Blade slap noise
  • Blade-vortex interaction
  • Helicopters
  • Noise prediction
  • Rotary wings
  • Wind tunnel tests
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 95-0750-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.26:198590
OCLC
marcive33450830
Author
Devenport, William J.
Title
Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions [microform] : semi-annual report to NASA Langley for worked performed under the grant / principal investigators: William J. Devenport, Stewart A.L. Glegg.
Imprint
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
NASA contractor report ; NASA CR-198590
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.
Added Author
Glegg, Stewart A. L.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:198590
Research Call Number
READEX Microfiche NAS 1.26:198590
View in Legacy Catalog