A Simple Theoretical Analysis and Experimental Investigation of Burning Processes for Stick Propellant

Abstract

The interior ballistic performance of propelling charges employing perforated unslotted stick propellant often cannot be simulated using either lumped-parameter or two-phase flow models without altering input data beyond realistic limits. In this work, a lumped-parameter model has been modified to account for enhanced burning within the perforations of stick propellant, a consequence of higher local pressures accompanying the choking of product gases exiting the perforations. A further extension allows treatment of additional surface area exposed should grain fracture occur as a result of excessive internal pressure. Results obtained using the modified code are compared to 155- mm howitzer firings. Data from closed-bomb firings which demonstrate the same effect are also included.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1983
Accession Number
ADA132968

Entities

People

  • Albert W. Horst
  • Frederick W. Robbins

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Artillery
  • Burning Rate
  • Closed Bomb Tests
  • Combustion
  • Engineering
  • Engineers
  • Flow
  • Gunpowder
  • Guns
  • Howitzers
  • Internal Pressure
  • Jet Propulsion
  • Military Research
  • Munitions
  • Propellants
  • Propelling Charges
  • Weapons

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Computational Modeling and Simulation
  • Rocket Propulsion.