Redesign of the Vulcain 2 Nozzle Extension-Reference-Cited by-同舟云学术

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Redesign of the Vulcain 2 Nozzle Extension

Published:2005-07-10 Issue: Volume: Page:
ISSN:
Container-title:41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Winterfeldt Lars-Olof,Laumert Björn,Tano Robert,James Philippe,Geneau Fabien,Blasi Roland,Hagemann Gerald

Publisher

American Institute of Aeronautics and Astronautics

Reference1 articles.

Cited by 23 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Mechanisms Contributing to the Dynamic Stability of a Flexible Subscale Rocket Nozzle;Journal of Propulsion and Power;2024-01

2. Computations of Side Loads in a Thrust-Optimized Parabolic Nozzle During High-Altitude Testing;AIAA Journal;2021-06

3. Computational Investigations of Side-Loads in a Thrust-Optimized Parabolic Nozzle during High-Altitude Testing;AIAA Scitech 2020 Forum;2020-01-05

4. Computational investigation of flow separation in a thrust-optimized parabolic nozzle during high-altitude testing;Computers & Fluids;2020-01

5. A new Metallic Thermal Barrier Coating System for Rocket Engines: Failure Mechanisms and Design Guidelines;Journal of Thermal Spray Technology;2019-08-05

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