Research Catalog

Title

Investigation of the effects of pressure gradient, temperature, and wall temperature ratio on the stagnation point heat transfer for circular cylinders and gas turbine vanes [microform] / by H.T. Nagamatsu and R. E. Duffy.

Author

Nagamatsu, H. T.

Publication

Troy, N.Y. : Rensselaer Polytechnic Institute, [1984]

Details

Additional Authors

• Duffy, R. E.
• Rensselaer Polytechnic Institute.
• Lewis Research Center.

Description

iii, 39 p. : ill.

Series Statement

NASA contractor report ; 174667

Uniform Title

NASA contractor report ; NASA CR-174667.

Subject

• Circular cylinders
• Gas turbines
• Heat flux
• Heat transfer
• High pressure
• Pressure gradients
• Shock tubes
• Vanes

Note

• "April 1984."
• "Prepared for National Aeronautics and Space Administration, Lewis Research Center under grant no. NAS3-292."

Bibliography (note)

• Includes bibliographical references (p. 36-39).

Reproduction (note)

• Microfiche.

Call Number

GPO Microfiche NAS 1.26:174667

OCLC

marcive688604806

Author

Nagamatsu, H. T.

Title

Investigation of the effects of pressure gradient, temperature, and wall temperature ratio on the stagnation point heat transfer for circular cylinders and gas turbine vanes [microform] / by H.T. Nagamatsu and R. E. Duffy.

Imprint

Troy, N.Y. : Rensselaer Polytechnic Institute, [1984]

Series

NASA contractor report ; 174667

NASA contractor report ; NASA CR-174667.

Bibliography

Includes bibliographical references (p. 36-39).

Reproduction

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1984. 1 microfiche.

Added Author

Duffy, R. E.

Rensselaer Polytechnic Institute.

Lewis Research Center.

Other Form:

Online version: Nagamatsu, H. T. Investigation of the effects of pressure gradient, temperature, and wall temperature ratio on the stagnation point heat transfer for circular cylinders and gas turbine vanes. (OCoLC)688609638

Gpo Item No.

0830-H-14 (MF)

Sudoc No.

NAS 1.26:174667