Review of two methods for calculating explosive Air blast

Jeffrey M. K. Chock, R. Kapania
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引用次数: 27

Abstract

Blast profiles and two primary methods of determining them are reviewed for use in the creation of a computer program for calculating blast pressures, which serves as a design tool to aid engineers or analysts in the study of structures subjected to explosive air blast. These methods were integrated into the computer program BLAST.F to generate air blast pressure profiles by one of two methods, that of the Army's Explosions in Air manual and a method outlined by Kingery and Bulmash in their work. These methods were compared after the creation of the program and can conservatively model the effects of spherical air blast and hemispherical surface burst. The code BLAST.F was used in conjunction with a commercial finite element code (NASTRAN) in a demonstration of method on a 30 by 30-inch aluminum 2519 quarter plate of fixed boundary conditions in hemispherical ground burst and showed good convergence with 256 elements for deflection and good agreement in equivalent stresses of a point near the blast between the 256 and 1024 element examples. Application of blasts to a hypothetical wing composed of aluminum 7075-T6 was also conducted showing good versatility of method for using this program with other finite element models.
爆炸性空气爆炸的两种计算方法综述
本文回顾了爆炸剖面和确定爆炸剖面的两种主要方法,以用于创建计算爆炸压力的计算机程序,该程序可作为设计工具,帮助工程师或分析人员研究受爆炸性空气爆炸影响的结构。这些方法被集成到计算机程序BLAST中。F用两种方法中的一种来产生空气爆炸压力曲线,一种是陆军的《空中爆炸》手册,另一种是金格里和布尔马什在他们的工作中概述的方法。在编制程序后,对这两种方法进行了比较,可以较为保守地模拟球形空气爆破和半球形表面爆破的效果。代码BLAST。F与商业有限元代码(NASTRAN)结合使用,在半球形地爆固定边界条件下的30 × 30英寸2519铝四分之一板上进行了方法演示,结果表明,256个单元的挠度与256个单元的挠度具有良好的收敛性,并且在爆炸附近点的等效应力方面,256个和1024个单元的例子之间具有良好的一致性。对7075-T6铝合金组成的假想机翼进行了爆破实验,表明该程序与其他有限元模型的通用性较好。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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