Title: An Empirical Formula for Stagnation Point Velocity Gradient for Spheres and Circular Cylinders in Hypersonic Flow
Abstract: When stagnation heat transfer rates are expressed in terms of free stream flow properties, the following combination of terms is found to occur: — where p s pressure at the stagnation point p ∞ free stream pressure U∞ free stream velocity D nose diameter ß stagnation point velocity gradient.
Publication Year: 1965
Publication Date: 1965-06-01
Language: en
Type: article
Indexed In: ['crossref']
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Cited By Count: 1
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