![](/img/cover-not-exists.png)
Wall Temperature and Prandtl Number Effects on Turbulent Boundary Layer Thicknesses and Shape Factors for Subsonic Compressible Gas Flow Over a Flat Plate
Kelnhofer, W. J.Volume:
91
Language:
english
Journal:
Journal of Engineering for Gas Turbines and Power
DOI:
10.1115/1.3574748
Date:
October, 1969
File:
PDF, 1.68 MB
english, 1969