Research Catalog

Experimental study of the effects of reynolds number on high angle of attack aerodynamic characteristics of forebodies during rotary motion

Title
Experimental study of the effects of reynolds number on high angle of attack aerodynamic characteristics of forebodies during rotary motion [microform] / H. Pauley, J. Ralston, and E. Dickes.
Author
Pauley, H.
Publication
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors
  • Ralston, J.
  • Dickes, E.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA contractor report ; NASA CR-195033
Subject
  • Aerodynamic characteristics
  • Angle of attack
  • Dynamic characteristics
  • Forebodies
  • Pressure distribution
  • Reynolds number
  • Rotary stability
  • Wind tunnel tests
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 95-0615-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.26:195033
OCLC
marcive34141310
Author
Pauley, H.
Title
Experimental study of the effects of reynolds number on high angle of attack aerodynamic characteristics of forebodies during rotary motion [microform] / H. Pauley, J. Ralston, and E. Dickes.
Imprint
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
NASA contractor report ; NASA CR-195033
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.
Added Author
Ralston, J.
Dickes, E.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:195033
Research Call Number
READEX Microfiche NAS 1.26:195033
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