Research Catalog

Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades

Title: Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades [microform] / Vijay K. Garg and Raymond E. Gaugler.
Author: Garg, Vijay Kumar, 1938-
Publication: [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors

Description

1 v.

Series Statement

NASA technical memorandum ; 106954

Subject

Note

Distributed to depository libraries in microfiche.
Shipping list no.: 96-0021-M.

Reproduction (note)

Microfiche.

Call Number

READEX Microfiche NAS 1.15:106954

OCLC

marcive33973275

Author

Garg, Vijay Kumar, 1938-

Title

Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades [microform] / Vijay K. Garg and Raymond E. Gaugler.

Imprint

[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]

Series

NASA technical memorandum ; 106954

Reproduction

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.

Added Author

Gaugler, Raymond E.

United States. National Aeronautics and Space Administration.

Gpo Item No.

0830-D (MF)

Sudoc No.

NAS 1.15:106954

Research Call Number

READEX Microfiche NAS 1.15:106954

View in Legacy Catalog