Accession Number:
AD0272641
Title:
AN APPROXIMATE STREAMTUBE METHOD TO DETERMINE THE EQUILIBRIUM FLOW FIELD ABOUT A BLUNT BODY TRAVELING AT SUPERSONIC SPEEDS
Descriptive Note:
Corporate Author:
ARMY ORDNANCE MISSILE COMMAND REDSTONE ARSENAL ALA
Personal Author(s):
Report Date:
1961-08-01
Pagination or Media Count:
1.0
Abstract:
An approximate streamtube method is presented to determine the flow field in the frontal portion of a spherical body under the assumption that the gas is in thermodynamic equilibrium. Numerical results of this method are compared with a previously determined solution. Author