基于特征法的火箭喷管形状设计优化方法

IF 1.8 Q2 ENGINEERING, AEROSPACE

CEAS Space Journal Pub Date : 2023-07-08 DOI:10.1007/s12567-023-00511-1

T. Fernandes, Alain Souza, F. Afonso

引用次数: 0

摘要

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A shape design optimization methodology based on the method of characteristics for rocket nozzles

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来源期刊

CEAS Space Journal ENGINEERING, AEROSPACE-

CiteScore

3.90

自引率

7.10%

发文量

期刊介绍： The CEAS Space Journal has been created by the CEAS Space Branch to provide an appropriate platform for the excellent scientific publications submitted by scientists and engineers. Under the umbrella of CEAS, the German Aerospace Center (DLR) and the European Space Agency (ESA) support the Journal. The Journal is devoted to new developments and results in all areas of space-related science and technology, including important spin-off capabilities and applications as well as ground-based support systems and manufacturing advancements. Of interest are also (invited) in-depth reviews of the status of development in specific areas of relevance to space, and descriptions of the potential way forward. Typical disciplines of interest include mission design and space systems, satellite communications, aerothermodynamics (including physical fluid dynamics), environmental control and life support systems, materials, operations, space debris, optics, optoelectronics and photonics, guidance, navigation and control, mechanisms, propulsion, power, robotics, structures, testing and thermal issues and small satellites. The Journal publishes peer-reviewed original articles, (invited) reviews and short communications.