SOLUTION OF THE PROBLEM OF A HYPERSONIC GAS FLOW AROUND AN ELONGATED BLUNTED BODY BY THE G. G. CHERNYI APPROXIMATE METHOD (RESHENIE ZADACHI OBTEKANIYA GIPERZVUKOVYM POTOKOM GAZA UDLINENNOGO ZATUPLENNOGO TELA PRIBLIZHENNYM METODOM G. G. CHERNOGO),

Abstract

The flow field around an axisymmetric body at zero angle of attack was studied analytically using Chernyy's method of approximation. The analysis is valid for streamlines inclined at shallow angles, and hence the solution is limited to a region aft of the blunt tip of the body. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 03, 1967
Accession Number
AD0670896

Entities

People

  • S. S. Grigoryan

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Flow
  • Flow Fields
  • Gas Flow

Readers

  • Fluid Dynamics.
  • Information Retrieval

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers