MODELING TECHNIQUE FOR HEAT TRANSFER SIMILARITY PROBLEMS AT HIGH SPEEDS

Abstract

A general method for the analysis of the heat transfer on bodies flying at very high speed is presented. In Part I, a modeling technique relative to the use of the blowdown supersonic and hypersonic wind tunnel to solve the complete similarity problems is given. In Part II, an application of the above technique is presented,AND EXPERIMENTAL RESULTS OF TURBULENT HEAT TRANSFER COEFFICIENTS ON BLUNT BODIES AT Mach Numbers 3.98 and 4.01 are presented. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1961
Accession Number
AD0262099

Entities

People

  • Giorgio Ravelli
  • Luigi Broglio

Organizations

  • Sapienza University of Rome

Tags

DTIC Thesaurus Topics

  • Blowdown
  • Blunt Bodies
  • Bodies
  • Coefficients
  • Heat Transfer
  • Heat Transfer Coefficients
  • Hypersonic Wind Tunnels
  • Mach Number
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow