CALCULATION OF HEAT TRANSFER ON FRONTAL SURFACE OF BLUFF BODY IN HYPERSONIC FLOW

Abstract

Viscous hypersonic flow at high Reynolds numbers over a blunt-nosed body is considered on the basis of Navier-Stokes equations. An asymptotic solution of the Navier-Stokes equations is obtained for the case where substantial viscous effects are present in the entire inner layer. A distinctive feature of the boundary value problem considered is that it contains a new similarity parameter.

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Document Details

Document Type
Technical Report
Publication Date
Nov 14, 1968
Accession Number
AD0683953

Entities

People

  • V. Ya. Neyland
  • Yu. N. Ermak

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Asymptotic Series
  • Boundaries
  • Boundary Layer
  • Boundary Value Problems
  • Compression
  • Equations
  • Euler Equations
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Heat Transfer
  • Heat Transmission
  • Hypersonic Flow
  • Pressure Gradients
  • Shock
  • Shock Waves
  • Viscous Flow

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers