One Approximate Method for Calculating the Aerodynamic Characteristics of Smooth Bodies, Streamlined at Different Angles of Attack by a Supersonic Flow of Gas,

Abstract

An approximation method of equivalent cones is examined for the calculation of the aerodynamic characteristics of smooth bodies in a supersonic flow of gas.

Document Details

Document Type
Technical Report
Publication Date
Jan 17, 1975
Accession Number
ADA006693

Entities

People

  • N. A. Makhin
  • V. F. Syagaev

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Flow
  • Supersonic Flow

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow