Research Catalog

Evaluation of panel code predictions with experimental results of inlet performance for a 17-inch ducted prop/fan simulator operating at mach 0.2

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 [microform] / D. R. Boldman ... [et al.].
Publication
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]

Details

Additional Authors
  • Boldman, D. R.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA technical memorandum ; 104428
Subject
  • Ducts
  • Engine inlets
  • Low speed wind tunnels
  • Panel method (Fluid dynamics)
  • Shrouded propellers
  • Simulators
  • Subsonic speed
Note
  • Distributed to depository libraries in microfiche.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:104428
OCLC
marcive32358654
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 [microform] / D. R. Boldman ... [et al.].
Imprint
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
Series
NASA technical memorandum ; 104428
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.
Added Author
Boldman, D. R.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:104428
Research Call Number
READEX Microfiche NAS 1.15:104428
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