SEPARATION TEST OF THE 1/22 SCALE TFD FROM THE F-105D AIRCRAFT AT THE GENERAL DYNAMICS HIGH SPEED WIND TUNNEL.

Abstract

A simulated separation test of a tactical fighter dispenser munition from an F-105D parent aircraft was conducted using a captive trajectory system. Test variables included Mach number and launch conditions. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1967
Accession Number
AD0838572

Entities

People

  • Robert F. Mcginnis

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Dispensers
  • Dynamics
  • Mach Number
  • Munitions
  • Trajectories
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Engineering