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Design of thrust augmentation control schedule during mode transition for turbo-ramjet engine

  • Published:2023-07 Issue: Volume:138 Page:108352
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Xi ZhihuaORCID,Zhang Haibo,Chen Ming,Cai Changpeng,Wang Jian

Funder

Natural Science Foundation of Jiangsu Province

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

1. Turbine based combination cycle (TBCC) propulsion subsystem integration;Snyder,2013

2. Highly reusable space transportation system study;Haney;AIP Conf. Proc.,1997

3. High speed aircraft/combined power integration analysis;Hu,2021

4. Turbine-based combined cycle propulsion system integration concept design;Chen;Proc. Inst. Mech. Eng., G J. Aerosp. Eng.,2013

5. Combined cycle propulsion: aerojet innovations for practical hypersonic vehicles;Bulman,2011
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