Tables For Supersonic Flow Around Right Circular Cones At Zero Angle Of Attack With List Of References
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Tables for Supersonic Flow of Helium Around Right Circular Cones at Zero Angle of Attack
The results of the calculation of supersonic flow of helium about right circular cones at zero angle of attack are presented in tabular form. The calculations were performed using the Taylor-Maccoll theory. Numerical integrations were performed using a Runge-Kutta method for second-order differential equations. Results were obtained for cone angles from 2.5 to 30 degrees in regular increments of 2.5 degrees. In all calculations the desired free-stream Mach number was obtained to five or more significant figures.
Monthly Catalog, United States Public Documents
Author: United States. Superintendent of Documents
language: en
Publisher:
Release Date: 1973
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.