CONSTANT ACCELERATION FLOWS AND APPLICATIONS TO HIGH-SPEED GUNS

Abstract

Solutions for isothermal, isentropic, and constant Mach number (at a specified location) flows with constant acceleration are obtained. It is shown that in application to high-speed guns, these solutions necessitate variable gun geometry or heating of the propellant; both requirements are considered at present impractical. Numerical solutions which give constant projectile acceleration in a fixed geometry gun are computed for ideal and real hydrogen propellant. Using the latter, and the appropriate similarity parameters, as well as practical constraints related to gun and projectile geometry and strength, it is shown that a substantial increase in muzzle velocity could be obtained if the constant base pressure cycle were more closely approximated in actual launchings. At present the velocity attained with large caliber guns is much smaller than with the small ones. In this connection, the validity of linear scaling of guns and the resulting possibility of application of small- scale developments to large caliber guns are indicated.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1966
Accession Number
AD0642333

Entities

People

  • J. Lukasiewicz

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Base Pressure
  • Computational Science
  • Contracts
  • Equations
  • Geometry
  • Hydrogen
  • Launch Tubes
  • Launching
  • Mach Number
  • Mass Flow
  • Materials
  • Muzzle Velocity
  • Pressure Distribution
  • Projectiles
  • Propellants

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Systems Analysis and Design
  • ballistics.