Award Date

1-1-2002

Degree Type

Dissertation

Degree Name

Doctor of Philosophy (PhD)

Department

Mechanical Engineering

First Committee Member

Darrell W. Pepper

Number of Pages

115

Abstract

The Joint Actinide Shock Physics Experimental Research (JASPER) facility utilizes a two-stage light gas gun to conduct equation of state experiments. The gun has a launch tube bore diameter of 28 mm, and is capable of launching projectiles at a velocity of 7.4 km/s using compressed hydrogen as a propellant. A numerical study is conducted to determine what effects, if any, launch tube exit geometry changes have on attitude of the projectile in flight. A comparison of two launch tube exit geometries is considered. The first case is standard muzzle geometry where the wall of the bore and the outer surface of the launch tube form a 90 degree angle. The second case includes a 26.6 degree bevel transition from the wall of the bore to the outer surface of the launch tube. The finite element method is employed to model the Euler equations and the compressible Navier-Stokes equations. The numerical method incorporates the use of trilinear, hexahedral, isoparametric elements, as well as the use of Petrov-Galerkin weighting applied to the advection terms. Mass lumping allows an explicit Euler scheme to be used in conjunction with a second-order Runge-Kutta approximation to advance the discretized equations in time. An h-adaptive mesh refinement scheme based on elemental flow feature gradients is utilized for greater solution accuracy. For both cases, solutions are calculated for several positions downstream of the launch tube exit. Numerical solutions obtained indicate that both cases will have an adverse effect on flight attitude of the projectile, with the beveled muzzle geometry performing worse than the standard case.

Keywords

Adaptive; Applied; Compressible; Compressible Flow; Computational Fluid Dynamics; Design; Element; Finite; Flow; Gas; Gun H-adaptive Finite Element; H-adaptive Finite Element; Light; Light-gas Gun; Solver

Controlled Subject

Mechanical engineering

File Format

pdf

File Size

2334.72 KB

Degree Grantor

University of Nevada, Las Vegas

Language

English

Permissions

If you are the rightful copyright holder of this dissertation or thesis and wish to have the full text removed from Digital Scholarship@UNLV, please submit a request to digitalscholarship@unlv.edu and include clear identification of the work, preferably with URL.

Rights

IN COPYRIGHT. For more information about this rights statement, please visit http://rightsstatements.org/vocab/InC/1.0/

Download


Share

COinS