首页> 美国政府科技报告 >Vibration Characteristics of Z-Ring-Stiffened 60 Deg Conical Shell Models of a Planetary Entry Spacecraft

【24h】

Vibration Characteristics of Z-Ring-Stiffened 60 Deg Conical Shell Models of a Planetary Entry Spacecraft

机译：Z型环加固60度锥形壳行星式航天器的振动特性

获取原文

页面导航

著录项
相似文献
相关主题

著录项

作者
Naumann, E. C.; Mixon, J. S.;
展开▼
作者单位

展开▼
年度 1971
页码 1-5
总页数 5
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Conical shells ; Spacecraft design ; Structural analysis ; Vibration tests ; Frequency response ; Reinforcement (structures) ; Stiffening;

机译：锥形壳;航天器设计;结构分析;振动试验;频率响应;加固（结构）;加强;

相似文献

外文文献
中文文献
专利

1. Free vibrational characteristics of GNP-reinforced joined conical-conical shells with different boundary conditions [J] . Damercheloo Ali Reza, Khorshidvand Ahmad Reza, Khorsandijou S. Mahdi, Thin-Walled Structures . 2021,第Deca期

机译：GNP加固的自由振动特性与不同边界条件的加固连接锥形果壳
2. Vibrational characteristic of FG porous conical shells using Donnell's shell theory [J] . Trends in Ecology & Evolution . 2020,第2期

机译：唐纳尔壳理论富孔锥形壳的振动特性
3. Vibrational characteristic of FG porous conical shells using Donnell's shell theory [J] . Yan Kai, Zhang Yao, Cai Hao, Steel & Composite Structures: An International Journal . 2020,第2期

机译：唐纳尔壳理论富孔锥形壳的振动特性
4. FREE VIBRATION CHARACTERISTICS OF SANDWICH CONICAL SHELLS WITH FGM FACE SHEETS: A FINITE ELEMENT APPROACH [C] . Tripuresh Deb Singha, Apurba Das, Gopal Agarwal, ASME gas turbine India conference . 2019

机译：带有FGM面片的夹心圆锥壳的自由振动特性：有限元方法
5. Analytical theories for spacecraft entry into planetary atmospheres and design of planetary probes [D] . Saikia, Sarag J. 2015

机译：航天器进入行星大气的分析理论和行星探测器的设计
6. The Dynamic Response and Vibration of Functionally Graded Carbon Nanotube-Reinforced Composite (FG-CNTRC) Truncated Conical Shells Resting on Elastic Foundations [O] . Duc Nguyen Dinh, Pham Dinh Nguyen 2017

机译：功能梯度碳纳米管增强复合材料（FG-CNTRC）截断的圆锥形壳体基于弹性基础的动力响应和振动
7. FREE VIBRATION ANALYSIS OF JOINED COMPOSITE CONICAL-CONICAL-CONICAL SHELLS CONTAINING FLUID [O] . Vu Quoc Hien, Tran Ich Thinh, Nguyen Manh Cuong, 2016

机译：加入含有流体的连接复合锥锥圆锥壳的自由振动分析
8. Vibration characteristics of Z-ring-stiffened 60 deg conical shell models of a planetary entry spacecraft [R] . Naumann, E. C., Mixon, J. S. 1971

机译：行星入口航天器Z形环加强60度锥壳模型的振动特性

Vibration Characteristics of Z-Ring-Stiffened 60 Deg Conical Shell Models of a Planetary Entry Spacecraft

著录项

相似文献

相关主题

期刊订阅