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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 /

Bibliographic Details
Main Author: Nagamatsu, H. T.
Corporate Authors: Rensselaer Polytechnic Institute, Lewis Research Center
Other Authors: Duffy, R. E.
Format: Government Document eBook
Language:English
Published: Troy, N.Y. : Rensselaer Polytechnic Institute, [1984]
Series:NASA contractor report ; NASA CR-174667.
Subjects:
Circular cylinders.
Gas turbines.
Heat flux.
Heat transfer.
High pressure.
Pressure gradients.
Shock tubes.
Vanes.
Online Access:https://purl.fdlp.gov/GPO/gpo1554
Description
Item Description:"April 1984."
"Prepared for National Aeronautics and Space Administration, Lewis Research Center under grant number NAS3-292."
Electronic resource.
Physical Description:1 online resource (iii, 39 pages) : digital, PDF file.
Bibliography:Includes bibliographical references (pages 36-39).