Insights into thermodynamic performance of a hypersonic precooled air-breathing engine with a complicated multi-branch closed cycle
Author:
Funder
Beihang University
Publisher
Elsevier BV
Reference48 articles.
1. Balepin V. High speed propulsion cycles. Advances on propulsion technology for high-speed aircraft. Neuilly-sur-Seine: RTO; 2007.
2. Snyder L, Escher D, DeFrancesco R, et al. Turbine Based Combination Cycle (TBCC) propulsion subsystem integration. Reston: AIAA; 2004. Report No.: AIAA-2004-3649.
3. Olds J, Bradford J, Olds J, et al. SCCREAM (Simulated Combined-Cycle Rocket Engine Analysis Module) - A conceptual RBCC engine design tool. Reston: AIAA; 1997. Report No.: AIAA-1997-2760.
4. Calvo W, Christensen K, Fedun M. Solid fuel gas generator air. Reston: AIAA; 1986. Report No.: AIAA-1986-1682.
5. Siebenhaar A, Bogar T. Integration and vehicle performance assessment of the aerojet “TriJet” combined-cycle engine. Reston: AIAA; 2009. Report No.: AIAA-2009-7420.
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