On the Drag of a Sphere at Extremely High Speeds
- 1 February 1958
- journal article
- Published by AIP Publishing in Journal of Applied Physics
- Vol. 29 (2) , 194-195
- https://doi.org/10.1063/1.1723065
Abstract
The formula for the pressure-drag coefficient of a sphere which moves at extremely high speeds is derived. In the derivation it is assumed that the nose of the shock contour follows exactly the frontal half of the spherical surface and the local pressure on the frontal spherical surface corresponds to the pressure behind the shock wave after the statistical equilibrium between the various degrees of freedom of the molecule has been reached. The chemical dissociation of the molecules behind the shock wave is taken into account in the analysis. The theoretical results of the drag coefficient of the spheres agree with the corresponding available measured value within the experimental error for the range of Mach number between 5 and 10.This publication has 3 references indexed in Scilit:
- The Drag Coefficient of Very High Velocity SpheresJournal of the Aeronautical Sciences, 1957
- Supersonic Drag of Spheres at Low Reynolds Numbers in Free FlightJournal of Applied Physics, 1957
- The Aerodynamic Performance of Small Spheres from Subsonic to High Supersonic VelocitiesJournal of the Aeronautical Sciences, 1945