Wing-Tail Interference Experiments at Supersonic Speeds

Abstract

Aerodynamic theory as applied to the design of supersonic missile configuration is discussed. Emphasis is placed on the study of aerodynamic interference parameters among the elemental low aspect ratio wing-body-tail combinations.

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Document Details

Document Type
Technical Report
Publication Date
Mar 15, 1963
Accession Number
AD0423302

Entities

People

  • John B. Wainwright

Organizations

  • University of Southern California

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerospace Craft
  • Aircrafts
  • Airplanes
  • Aspect Ratio
  • California
  • Lifting Surfaces
  • Mach Number
  • Measurement
  • Procurement
  • Tank Guns
  • Trailing Edges
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Theoretical Analysis.

Technology Areas

  • Hypersonics