Yaw Card Range Tests of a 30mm Target Projectile

Abstract

Experimental results of yaw card range tests with 30mm target projectiles are presented. Results include experimentally determined static and dynamic stability derivatives and drag coefficients obtained at a free-flight Mach number of 3.0.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1976
Accession Number
ADB014108

Entities

People

  • Kenneth O. West

Tags

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Angular Motion
  • Circuits
  • Coefficients
  • Data Analysis
  • Data Reduction
  • Equations
  • Explosives
  • Flight
  • Flight Paths
  • Free Flight
  • Instrumentation
  • Mach Number
  • Measurement
  • Projectiles
  • Test And Evaluation

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Fluid Dynamics.
  • ballistics.