Tables for Supersonic Flow of Helium Around Right Circular Cones at Zero Angle of Attack

Tables for Supersonic Flow of Helium Around Right Circular Cones at Zero Angle of Attack
Author: Joseph L. Sims
Publisher:
Total Pages: 36
Release: 1973
Genre: Aerodynamics, Supersonic
ISBN:

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.

Report to the Congress

Report to the Congress
Author: United States. National Aeronautics and Space Administration
Publisher:
Total Pages: 572
Release: 1965
Genre:
ISBN:

NASA Scientific and Technical Reports

NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
Total Pages: 1152
Release: 1965
Genre: Aeronautics
ISBN: