NEW APPROACH TO THE TWO-DIMENSIONAL HYPERSONIC BLUNT BODY PROBLEM.

Abstract

Hypersonic flow past a two-dimensional blunt body was treated by making use of the technique of the perturbation of independent variables. Application to a flat plate normal to the oncoming flow leads us to the same results as those obtained by Cole and Brainerd due to a different procedure. One more term is found for the stand-off distance of a shock wave. The case past an arbitrary body is also considered. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1965
Accession Number
AD0615901

Entities

People

  • Kinzo Hida

Organizations

  • University of Cincinnati

Tags

DTIC Thesaurus Topics

  • Blunt Bodies
  • Bodies
  • Flow
  • Hypersonic Flow
  • Perturbations
  • Shock
  • Shock Waves
  • Two Dimensional
  • Waves

Fields of Study

  • Physics

Readers

  • Calculus or Mathematical Analysis
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers