Transonic Wind Tunnel Tests on a Missile Model with Canard Wings. Volume 3

Abstract

Volume 3 of a three volume report tabulates aerodynamic and thrust test data on a wind tunnel model of a guided missile with canard wings. Included are tail fin force and moment coefficients.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1973
Accession Number
AD0766661

Entities

People

  • R. E. De Kuyper

Organizations

  • Calspan

Tags

Communities of Interest

  • Advanced Electronics

DTIC Thesaurus Topics

  • Avionics
  • Computer Science
  • Corporations
  • Electronics
  • Research Facilities
  • Test Facilities
  • Transonic Wind Tunnels
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Business Analytics