Research Catalog

Computational prediction of isolated performance of an axisymmetric nozzle at Mach number 0.90

Title: Computational prediction of isolated performance of an axisymmetric nozzle at Mach number 0.90 [microform] / John R. Carlson.
Author: Carlson, John R.
Publication: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

Details

Additional Authors

Langley Research Center.

Description

1 v.

Series Statement

NASA technical memorandum ; 4506

Subject

Note

Distributed to depository libraries in microfiche.
Shipping list no.: 94-0415-M.

Reproduction (note)

Microfiche.

Call Number

READEX Microfiche NAS 1.15:4506

OCLC

marcive31095890

Author

Carlson, John R.

Title

Computational prediction of isolated performance of an axisymmetric nozzle at Mach number 0.90 [microform] / John R. Carlson.

Imprint

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]

Series

NASA technical memorandum ; 4506

Reproduction

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.

Added Author

Langley Research Center.

Gpo Item No.

0830-D (MF)

Sudoc No.

NAS 1.15:4506

Research Call Number

READEX Microfiche NAS 1.15:4506

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