Transonic Wind Tunnel Tests on a Missile Model with Canard Wings. Volume 2

Abstract

The report is Volume 2 of a three volume series. Tables of aerodynamic test data are given, including balance cavity and base pressure coefficients, axial force for aerodynamic and thrust phases, canard position, and force and moment coefficients for a series of runs.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1973
Accession Number
AD0766660

Entities

People

  • R. E. De Kuyper

Organizations

  • Calspan

Tags

Communities of Interest

  • Advanced Electronics

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Research Facilities
  • Test Facilities
  • Transonic Wind Tunnels
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Business Analytics
  • Fluid Dynamics.