Photothermoviscoelastic Analysis of a Case Bonded Rocket Grain

机译：一例结合火箭纹的光热粘弹性分析

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

An experimental program was performed to obtain meaningful data on transient thermal stresses in a case bonded circular port rocket grain model for correlation with theory. Both the experimental procedure and the theory were developed as part of the program. Consequently the reliability of the experimental data ultimately must await comparison of the data with the newly developed theory. The data reveal the progress of the thermal stress field from the inception upon a cold (and essentially elastic) grain through the transition to a warm (and principally viscoelastic) grain. The data were reproducible and are considered to be scientifically meaningful (Author)

著录项

作者
Becker, H.; Colao, A.;
展开▼
作者单位

展开▼
年度 1962
页码 p.1-2
总页数 2
原文格式 PDF
正文语种 eng
中图分类
关键词
ROCKET PROPELLANT GRAINS ; THERMAL STRESSES ; SOLID ROCKET PROPELLANTS ; PHOTOELASTICITY ; VISCOELASTICITY ; THERMAL PROPERTIES ; MODELS (SIMULATIONS) ; EPOXY PLASTICS ; ISOCYANATE PLASTICS;

机译：火箭推进剂颗粒;热应力;固体火箭推进剂;光弹性;粘弹性;热性能;模型（模拟）;环氧塑料;异氰酸酯塑料;

相似文献

外文文献
中文文献
专利

1. Numerical analysis on combustion instabilities in end-burning-grain solid rocket motors utilizing pressure-coupled response functions [J] . Aerospace science and technology . 2020,第Mara期

机译：基于压力耦合响应函数的端燃烧颗粒固体火箭发动机燃烧不稳定性的数值分析
2. Three-dimensional numerical analysis on combustion performance and flow of hybrid rocket motor with multi-segmented grain [J] . Hui TIAN, Yu DUAN, Hao ZHU 中国航空学报（英文版） . 2020,第004期

机译：多段混合动力火箭发动机燃烧性能和流量的三维数值分析
3. Modeling and analysis of triggering pulse to thermoacoustic instability in an end-burning-grain model solid rocket motor [J] . Fi Shixiang, Wang Bing Aerospace science and technology . 2019,第Deca期

机译：燃烧尾波模型固体火箭发动机中热声不稳定性触发脉冲的建模与分析
4. Assessing the ageing-state of solid propellant grains in case-bonded rocket motors by measuring bondline stresses [C] . Gunter Mussbach, Giuseppe Tussiwand, Jim Buswell International Annual Conference of ICT . 2015

机译：通过测量粘合线应力，评估壳体粘合火箭电机中固体推进剂颗粒的老化状态
5. Development of a rocket motor test system and a study of hybrid rocket fuel grains. [D] . Patterson, William Ray. 2009

机译：火箭发动机测试系统的开发和混合火箭燃料颗粒的研究。
6. Potential of Brewer’s Spent Grain as a Potential Replacement of Wood in pMDI UF or MUF Bonded Particleboard [O] . Marius Cătălin Barbu, Zeno Montecuccoli, Jakob Förg, 2021

机译：酿酒师花了谷物的潜力作为PMDIUF或MUF粘合刨花板的潜在替代木材
7. DESIGN QUALIFICATION OF A SINGLE-GRAIN ROCKET MOTOR FOR SHELF LIFE EXTENSION PROGRAM OF MULTI-GRAIN ROCKET MOTOR [O] . M. Sammour, H. Mostafa 2007

机译：多粒火箭电机货物寿命扩展程序单粒火箭电机的设计资格
8. Development of Experimental Stress Analysis Methods to Determine Stresses and Strains in Solid Propellant Grains. Stresses in a Split Cylinder Bonded to a Case and Subjected to Restrained Shrinkage [R] . Durelli, A. J., Parks, V. J., Lee, H. C. 1968

机译：确定固体推进剂颗粒应力和应变的实验应力分析方法的发展。分离式气缸中的应力与外壳粘合并受到约束收缩

Photothermoviscoelastic Analysis of a Case Bonded Rocket Grain

摘要

著录项

相似文献

相关主题

期刊订阅