Accession Number:

AD0493180

Title:

DEVELOPMENT OF HIGH SPEED AERODYNAMIC HEAT TRANSFER COEFFICIENTS FOR FLAT PLATES AND CONES,

Descriptive Note:

Corporate Author:

ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL AER OBALLISTICS DIRECTORATE

Personal Author(s):

Report Date:

1963-07-11

Pagination or Media Count:

30.0

Abstract:

The boundary layer on a flat plate for laminar and turbulent flow with an analysis of a current method to calculate aerodynamic heat transfer coefficients are presented. Specific heat variations of gas with temperatures up to dissociation are included with the aerodynamic heat transfer coefficient in a transient temperature digital program. The boundary layer and aerodynamic heat transfer coefficients developed for a flat plate may be applied to cone surfaces with the correction factors indicated in this report. Author

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE