Parametric analysis of thermal cycle of a short take-off and vertical landing engine
Author:
Affiliation:
1. School of Mechanical Engineering , Shanghai Jiao Tong University , Shanghai 200240 , P. R. China
2. Naval Research Institute , Shanghai 100084 , P. R. China
Abstract
Funder
National Natural Science Foundation of China
Chinese-German Center for Research Promotion
Publisher
Walter de Gruyter GmbH
Link
https://www.degruyter.com/document/doi/10.1515/tjj-2023-0054/pdf
Reference35 articles.
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3. Armstrong, FW, Levine, J. Overview of the US/UK ASTOVL program. SAE Technical Paper 872365; 1987.
4. Waesche, J, Migdal, D. High-perf orance jet-V/STOL development. J Aircraft 1977;14:97–103. https://doi.org/10.2514/3.58753.
5. Hooker, S. History of the Pegasus vectored thrust engine. J Aircraft 1981;18:322–6. https://doi.org/10.2514/3.44708.
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