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

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.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Apr 14, 2005
Accession Number
ADA447112

Entities

People

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

Organizations

  • Indian Institute of Science, Bengaluru

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Abstracts
  • Atmospheres
  • Boundaries
  • Boundary Layer
  • Carbon Dioxide
  • Computational Fluid Dynamics
  • Equations
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Fluid Flow
  • Friction
  • Heat Transfer
  • Hypersonic Flow
  • Mach Number
  • Skin Friction
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow