DID YOU KNOW? DTIC has over 3.5 million final reports on DoD funded research, development, test, and evaluation activities available to our registered users. Click
HERE to register or log in.
Accession Number:
ADA230901
Title:
A Comparison of Experimental and Numerical Blast Data for Perforated Muzzle Brakes
Descriptive Note:
Final rept.
Corporate Author:
ARMY ARMAMENT RESEARCH DEVELOPMENT AND ENGINEERING CENTER WATERVLIET NY BENET LABS
Report Date:
1990-12-01
Pagination or Media Count:
29.0
Abstract:
A perforated muzzle brake consists of a set of vents drilled through the wall of a canon near the muzzle, while venting reduces the axial thrust produced by the gas at the muzzle, thereby effecting a decrease in weapon impulse, the redirected exhaust increases blast levels upstream of the muzzle. The problem is to design a cannon brake system which yields specified values of muzzle velocity and weapon impulse but minimizes the blast increase. A numerical model of the blast field produced by a cannon having a perforated muzzle brake was previously developed. The results compared favorably with Dillons near-field shadowgraph data for a 20-mm cannon. This report describes improvements to the model and compares the predictions with free-field blast data for small and large caliber cannon. The results show good agreement with data for a 20-mm cannon and satisfactory agreement with data for 105-mm and 120-mm cannon.
Distribution Statement:
APPROVED FOR PUBLIC RELEASE