ADDITIONAL CALCULATIONS OF HYPERSONIC DYNAMIC STABILITY.

Abstract

Calculations of the hypersonic static and dynamic stability of ogive and ogive-cylinder fuselages, and of rectangular and delta wings in the presence of those fuselages, are presented. The results are compared with those calculated by Newtonian theory and by supersonic flow theories. A description is presented of wind tunnel models which are being constructed for tests to evaluate the predicted trends. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1964
Accession Number
AD0606203

Entities

People

  • Martin R. Fink

Organizations

  • United Aircraft Corporation

Tags

DTIC Thesaurus Topics

  • Airframes
  • Delta Wings
  • Flow
  • Fuselages
  • Mechanical Structure
  • Models
  • Supersonic Flow
  • Wind Tunnel Models
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow