The Resource Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic condition, Robert W. Hess ... [et al.], (microform)

Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic condition, Robert W. Hess ... [et al.], (microform)

Label
Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic condition
Title
Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic condition
Statement of responsibility
Robert W. Hess ... [et al.]
Contributor
Subject
Language
eng
Cataloging source
GPO
Government publication
federal national government publication
Index
no index present
Literary form
non fiction
http://library.link/vocab/relatedWorkOrContributorName
  • Hess, R. W.
  • Langley Research Center
Series statement
NASA technical memorandum
Series volume
89080
http://library.link/vocab/subjectName
  • Reynolds number
  • Mach number
  • Aerodynamics
Label
Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic condition, Robert W. Hess ... [et al.], (microform)
Instantiates
Publication
Note
Distributed to depository libraries in microfiche
Control code
17236370
Extent
1 v.
Form of item
microfiche
Reproduction note
Microfiche.
Label
Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic condition, Robert W. Hess ... [et al.], (microform)
Publication
Note
Distributed to depository libraries in microfiche
Control code
17236370
Extent
1 v.
Form of item
microfiche
Reproduction note
Microfiche.

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      39.77004 -86.164015

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