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Evaluation of a finite-element analysis for longitudinal vibrations of liquid propellant launch vehicles

机译：液体推进剂运载火箭纵向振动有限元分析评估

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摘要

Evaluation of finite element analysis for longitudinal vibrations of liquid propellant launch vehicle

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作者
Pinson, L. D.;
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年度 1970
页码 1-60
总页数 60
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
FINITE ELEMENT METHOD; LAUNCH VEHICLES; LIQUID PROPELLANT ROCKET ENGINES; LONGITUDINAL STABILITY; SATURN 5 LAUNCH VEHICLES; VIBRATION;

机译：有限元法;发射车辆;液体推进剂火箭发动机;纵向稳定性; saTURN 5 LUNCH车辆;振动;

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专利

1. Finite-Element Modeling and Frequency-Domain Analysis of Liquid-Propulsion Launch Vehicle [J] . Hao Yu, Tang Guo-an, Xu Deyuan, AIAA Journal . 2015,第11期

机译：液体推进运载火箭的有限元建模和频域分析
2. Experimental and Computational Modal Analyses for Launch Vehicle Models considering Liquid Propellant and Flange Joints [J] . Chang-Hoon Sim, Geun-Sang Kim, Dong-Goen Kim, International journal of aerospace engineering . 2018,第1期

机译：考虑液体推进剂和法兰接头的运载火箭模型的实验和计算模态分析
3. Experimental and Computational Modal Analyses for Launch Vehicle Models considering Liquid Propellant and Flange Joints [J] . Sim Chang-Hoon, Kim Geun-Sang, Kim Dong-Goen, International journal of aerospace engineering . 2018,第PTa1期

机译：考虑液体推进剂和法兰接头的运载火箭模型的实验和计算模态分析
4. Structural Modeling Reflected Nonlinearity for Longitudinal Dynamic Instability (POGO) Analysis of Liquid Propellant Launch Vehicles in Preliminary Design Phase [C] . JunBeom Kim, SangJoon Shin, JongHo Park, AIAA space and astronautics forum and exposition . 2015

机译：初步设计阶段液体动力运载火箭纵向动态不稳定性（POGO）分析的结构模型反射非线性
5. Experimental evaluation of vehicle cabin noise from suspension induced vibrations using transfer path and psychoacoustic analysis techniques. [D] . Radic, Nebojsa. 2008

机译：使用传递路径和心理声学分析技术对悬架引起的振动产生的车厢噪声进行实验评估。
6. Molecular impact of launch related dynamic vibrations and static hypergravity in planarians [O] . Nídia de Sousa, Marcello Caporicci, Jeroen Vandersteen, 2020

机译：普林斯人中发射相关动态振动和静态超高刻的分子影响
7. Solving the problem of minimax closed-loop control of liquid-propellant launch vehicle fuel consumption control [O] . A. F. Shorikov, V. I. Kalev 2020

机译：解决液体推进剂发射车燃料消耗控制的最小闭环控制问题
8. Evaluation of a Finite-Element Analysis for Longitudinal Vibrations of Liquid Propellant Launch Vehicles [R] . Pinson, L. D. 1970

机译：液体推进剂运载火箭纵向振动有限元分析

Evaluation of a finite-element analysis for longitudinal vibrations of liquid propellant launch vehicles

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