Research Catalog

An investigation of bleed configurations and their effect on shock wave/boundary layer interactions final report

Title
An investigation of bleed configurations and their effect on shock wave/boundary layer interactions [microform] : final report / Awatef Hamed, principal investigator.
Author
Hamed, A. (Awatef)
Publication
[Cincinnati, Ohio?] : University of Cincinnati ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors
United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA contractor report ; NASA CR-199439
Subject
  • Corner flow
  • Engine design
  • Engine inlets
  • Oblique shock waves
  • Secondary flow
  • Separated flow
  • Shock wave interaction
  • Supersonic inlets
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 96-0187-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.26:199439
OCLC
marcive34562841
Author
Hamed, A. (Awatef)
Title
An investigation of bleed configurations and their effect on shock wave/boundary layer interactions [microform] : final report / Awatef Hamed, principal investigator.
Imprint
[Cincinnati, Ohio?] : University of Cincinnati ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
NASA contractor report ; NASA CR-199439
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.
Added Author
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:199439
Research Call Number
READEX Microfiche NAS 1.26:199439
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