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

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE