Hypersonic Flow around a Thin Three-Dimensional Body,

Abstract

Hypersonic nonviscous flow about a thin three-dimensional body of triangular wing shape was investigated. In the framework of asymptotic theory of small perturbations, equations of motion and boundary conditions for the general class of perturbations were obtained. Flow about such a body is divided into two regions: an external region of uniform flow and a central region with conical flow. The first region is examined in the present paper. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 28, 1972
Accession Number
AD0744143

Entities

People

  • L. I. Dzvonyk

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Delta Wings
  • Equations
  • Equations Of Motion
  • Flow
  • Hypersonic Flow
  • Mathematics
  • Perturbations
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight