Research Catalog

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

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

Details

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