Accession Number:

ADA447112

Title:

Numerical and Experimental Analysis of Transpiration Cooling in Carbon Dioxide Atmosphere at Hypersonic Mach Numbers

Descriptive Note:

Conference paper

Corporate Author:

INDIAN INST OF SCIENCE BANGALORE DEPT OF AEROSPACE ENGINEERING

Personal Author(s):

• Kulkarni, V. N.
• Kulkarni, P. S.
• Reddy, K. P.

Report Date:

2005-04-14

Pagination or Media Count:

4.0

Abstract:

The numerical solutions are obtained for skin friction, heat transfer to the wall and growth of boundary layer along the flat plate by employing two dimensional Navier-Stokes equations governing the hypersonic flow coupled with species continuity equations. Flow fields have been computed along the flat plate in CO2 atmosphere in the presence of transpiration cooling using air and carbon dioxide.

Descriptors:

• *HEAT TRANSFER
• *NUMERICAL ANALYSIS
• *MACH NUMBER
• *SKIN FRICTION
• *HYPERSONIC FLOW
• *CARBON DIOXIDE
• INDIA
• BOUNDARY LAYER
• NAVIER STOKES EQUATIONS
• TRANSPIRATION
• FLOW FIELDS
• TWO DIMENSIONAL
• GROWTH(GENERAL)

Subject Categories:

• Numerical Mathematics
• Fluid Mechanics
• Thermodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE