Research Catalog

Effects of yaw and pitch motion on model attitude measurements

Title
Effects of yaw and pitch motion on model attitude measurements [microform] / Ping Tcheng, John S. Tripp, and Tom D. Finley.
Author
Tcheng, Ping.
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors
  • Tripp, John S.
  • FInley, Tom D.
  • Langley Research Center.
Description
1 v.
Series Statement
NASA technical memorandum ; 4641
Subject
  • Aircraft models
  • Angular velocity
  • Computational fluid dynamics
  • Dimensional measurement
  • Dynamic response
  • Mathematical models
  • Pitching moments
  • Wind tunnel tests
  • Yaw
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 95-0478-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:4641
OCLC
marcive32864042
Author
Tcheng, Ping.
Title
Effects of yaw and pitch motion on model attitude measurements [microform] / Ping Tcheng, John S. Tripp, and Tom D. Finley.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
NASA technical memorandum ; 4641
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.
Added Author
Tripp, John S.
FInley, Tom D.
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:4641
Research Call Number
READEX Microfiche NAS 1.15:4641
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