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