Thermoelastic Analysis of an Heterogeneous Orthotropic Nose Cap for a Hypersonic Vehicle

机译：高超声速车辆异质正交鼻帽的热弹性分析

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

Considering xz plane heterogeneous mechanical properties and thermal-pressure loads, thermoelastic analysis is applied on orthotropic nose cap of a hypersonic vehicle in the flight trajectory. The results show that the thermal-stress of sphere section presents annular, the Mises equivalent stress is of periodicity of 90° in tail so obviously that a reasonable connection is important. Finally, two connections, bolted and plug connection, are considered to relax the overnice tail constrains, and the results show that the plug connection is reasonable for the hypersonic heterogeneous orthotropic nose cap.

机译：考虑到XZ平面异质机械性能和热压载荷，在飞行轨迹中施加在超声波轨道的正交鼻帽上的热弹性分析。结果表明，球形截面的热应力呈现环形，误率等效应力在尾部的周期性为90°，显然合理的连接是重要的。最后，两种连接，螺栓和插头连接被认为是放宽过度尾部约束，结果表明，过度的异质正交鼻帽是合理的。

著录项

来源
《International Conference on Materials and Products Manufacturing Technology》|2011年||共10页
会议地点
作者
Xinghua Cheng; Tao Yang; Zhongdong Chang;
展开▼
作者单位

展开▼
会议组织
原文格式 PDF
正文语种
中图分类 TG17-532;
关键词
Orthotropic; Heterogeneous; Thermal Stress; Nose Cap;

机译：原位;异质;热应力;鼻梁;

相似文献

外文文献
中文文献
专利

1. Modeling of aerodynamic heat flux and thermoelastic behavior of nose caps of hypersonic vehicles [J] . Marina G. Persova, Yury G. Soloveichik, Vasiliy K. Belov, Acta astronautica . 2017,第JULa期

机译：高超音速飞行器鼻罩的空气动力学热通量和热弹性行为建模
2. 3D modeling of thermo-mechanical behavior of composite-made nose caps of hypersonic vehicles [J] . Soloveichik Yury G., Persova Marina G., Vagin Denis V., Applied thermal engineering: Design, processes, equipment, economics . 2016,第Null期

机译：高超声速飞行器复合材料鼻罩热机械行为的3D建模
3. Thermo-Structural Behaviour Prediction of the Nose Cap of a Hypersonic Vehicle Based on Multifield Coupling [J] . Xuewen Sun, Haibo Yang, Tao Mi International journal of aerospace engineering . 2020,第4期

机译：基于多牛耦合的超音速车辆鼻帽的热结构行为预测
4. Thermoelastic Analysis of an Heterogeneous Orthotropic Nose Cap for a Hypersonic Vehicle [C] . Xinghua Cheng, Tao Yang, Zhongdong Chang International Conference on Materials and Products Manufacturing Technology . 2011

机译：高超声速车辆异质正交鼻帽的热弹性分析
5. Design-oriented thermoelastic analysis, sensitivities, and approximations for shape optimization of aerospace vehicles. [D] . Bhatia, Manav. 2007

机译：面向设计的热弹性分析，灵敏度和近似值，用于航空航天器的形状优化。
6. Unconventionally Designed Tracking Loop Adaptable to Plasma Sheath Channel for Hypersonic Vehicles [O] . Lei Shi, Shurong Yuan, Bo Yao 2021

机译：非常规设计的跟踪环适用于超音速车辆的等离子护套通道
7. Numerical analysis of hypersonic flows around blunt-nosed models and a space vehicle [O] . Saldivar Massimi H, Shen H, Wen CY, 2015

机译：钝头模型和航天器周围高超声速流动的数值分析
8. Air Vehicle Integration and Technology Research (AVIATR). Delivery Order 0023: Predictive Capability for Hypersonic Structural Response and Life Prediction: Phase 2 - Detailed Design of Hypersonic Cruise Vehicle Hot- Structure. [R] . Zuchowski, B. 2012

机译：飞行器整合与技术研究（aVIaTR）。交货单0023：高超声速结构响应和寿命预测的预测能力：第2阶段 - 高超声速巡航车辆热结构的详细设计。

Thermoelastic Analysis of an Heterogeneous Orthotropic Nose Cap for a Hypersonic Vehicle

摘要

著录项

相似文献

相关主题

期刊订阅