Research Catalog

An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles

Title
An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles [microform] / Craig A. Hunter.
Author
Hunter, Craig A.
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors
Langley Research Center.
Description
1 v.
Series Statement
NASA contractor report ; 195050
Uniform Title
NASA contractor report ; NASA CR-195050.
Subject
  • Boundary layer equations
  • Compressible flow
  • Convergent-divergent nozzles
  • Mathematical models
  • Nozzle design
  • Nozzle efficiency
  • Nozzle flow
  • Performance prediction
  • Static thrust
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 95-0479-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.26:195050
OCLC
marcive32802365
Author
Hunter, Craig A.
Title
An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles [microform] / Craig A. Hunter.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
NASA contractor report ; 195050
NASA contractor report ; NASA CR-195050.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.
Added Author
Langley Research Center.
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:195050
Research Call Number
READEX Microfiche NAS 1.26:195050
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