ANALYSIS OF FLOW NEAR A BLUNT SOLID OF REVOLUTION AT ANGLE OF ATTACK IN SUPERSONIC FLOW OF GAS,

Abstract

A solution is given to the forward problem using integral relations with interpolation with respect to two variables.

Document Details

Document Type
Technical Report
Publication Date
Nov 30, 1965
Accession Number
AD0625236

Entities

People

  • A. N. Minailos

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Flow
  • Fluid Flow
  • Gas Flow
  • Integrals
  • Interpolation
  • Mathematics
  • Revolutions
  • Supersonic Flow

Fields of Study

  • Physics

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers