Research Catalog

Reduction of the shock wave intensity by modifying the transsonic [i.e. transonic] blade trailing edge

Title
Reduction of the shock wave intensity by modifying the transsonic [i.e. transonic] blade trailing edge [microform] / Piotr Doerffer.
Author
Doerffer, Piotr.
Publication
Washington, D.C. : National Aeronautics and Space Administration, [1983]

Details

Additional Authors
United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA technical memorandum ; NASA TM-77029
Alternative Title
Reduction of the shock wave intensity by modifying the transonic blade trailing edge
Subject
  • Shock waves > Diffraction
  • Aerodynamics, Transonic
  • Flow geometry
  • Shock wave propagation
  • Trailing edges
  • Transonic flow
Reproduction (note)
  • Microfiche.
Call Number
GPO Microfiche NAS 1.15:77029
OCLC
marcive234874298
Author
Doerffer, Piotr.
Title
Reduction of the shock wave intensity by modifying the transsonic [i.e. transonic] blade trailing edge [microform] / Piotr Doerffer.
Imprint
Washington, D.C. : National Aeronautics and Space Administration, [1983]
Series
NASA technical memorandum ; NASA TM-77029
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1984]. 1 microfiche.
Added Author
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:77029
Research Call Number
GPO Microfiche NAS 1.15:77029
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