Theory of Transonic Gas Guns.

Abstract

A review is given of analytical methods for predicting the muzzle velocity of compressed gas guns. Steady adiabatic expansion theory, quasi-steady theory and unsteady theory are all examined, with emphasis placed on simplified analytical methods applicable to subsonic and transonic muzzle velocities. New formulae are obtained and compared with numerical results from a full theoretical treatment of the gas flow. The comparisons show that the new analytic results are remarkably effective and can therefore be used for gun design. The effects of atmospheric counter pressure are treated separately and a new method of correcting the predicted velocity is given. An analysis of data from actual subsonic guns highlights the importance of muzzle pressure reflections in reducing the retarding pressure at low subsonic speeds. The observed muzzle velocities are about 10% below the muzzle velocities predicted by theory. Finally, nitrogen, helium and hydrogen are compared as potential driver gases for transonic guns. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1977
Accession Number
ADA051076

Entities

People

  • L. M. Sheppard

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force Facilities
  • Barrels
  • Boundary Layer
  • Compressors
  • Department Of Defense
  • Differential Equations
  • Engineering
  • Equations
  • Flow
  • Gas Compressors
  • Gas Flow
  • Gas Guns
  • Mach Number
  • Muzzle Velocity
  • Shock Waves
  • Waves
  • Weapons

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • ballistics.