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Title:
Evaluation of panel code predictions with experimental results of inlet performance for a 17-inch ducted prop/fan simulator operating at mach 0.2 /
D. R. Boldman [and others].
Publisher:
National Aeronautics and Space Administration,
Copyright Date:
1991
Description:
1 volume.
Reproduction Info:
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.
Subject:
Ducts.
Engine inlets.
Low speed wind tunnels.
Panel method (Fluid dynamics)
Shrouded propellers.
Simulators.
Subsonic speed.
Other Authors:
Boldman, D. R.
United States. National Aeronautics and Space Administration. http://id.loc.gov/authorities/names/n78087581
Notes:
Distributed to depository libraries in microfiche.
Series:
NASA technical memorandum ; 104428
OCLC:
(OCoLC)32358654
Locations:
OVUX522 --
University of Iowa Libraries
(Iowa City)
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