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Performance Characteristics of a TBCC Engine with Turbo-Ramjet Engine Transition Mode
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 Title & Authors
Performance Characteristics of a TBCC Engine with Turbo-Ramjet Engine Transition Mode
Moon, Kyoo-Hwan; Sung, Hong-Gye;
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The performance characteristics of a TBCC engine considering the transition mode from a turbojet to a ramjet engine has been investigated. The performance of each engine was proposed and a transition mode of the TBCC engine has been evaluated by adjusting the operating rate of the ramjet engine and turbojet engine performance changes continuously. Based on the transition model, it was confirmed that the performance is continuously changed at various flight Mach numbers and altitudes. The performance characteristics including thrust and specific impulse considering various flight conditions and transition mode were analyzed, which testifies characteristics of the engine itself, as well as transition of the combined cycle.
TBCC(Turbine Based Combined Cycle);Transition Mode;
 Cited by
재사용 발사체 및 미래추진기관 기술발전 전망 및 방향,김춘택;양인영;이경재;이양지;

한국항공우주학회지, 2016. vol.44. 8, pp.686-694 crossref(new window)
Technology Development Prospects and Direction of Reusable Launch Vehicles and Future Propulsion Systems, Journal of the Korean Society for Aeronautical & Space Sciences, 2016, 44, 8, 686  crossref(new windwow)
Sung, H. G., and Yoon, H. G., "Technical Review and Analysis of Ramjet/Scramjet Technology II.Scramjet and Combined Cycle Engine," KSPE, Vol. 10, No. 2, 2006, pp.115-128.

Noh, J. H., Choi, J. Y., Byun, J. R., Gil, H. Y., Yoon, H. G., and Lim, J. S., "DARPA's Hypersonic Vehicle and TBCC Engine Programs," KSPE, Vol. 14, No. 1, 2010, pp. 65-78.

Kobayashi, H., and Tanatsugu, N., "Optimization Method on TSTO Spaceplane System Powered by Airbreather," 2001, AIAA 2001-3965

Colville, J. R., Starkey, R. P., and Lewis, M. J., "Axisymmetric Inlet Design for Combined-Cycle Engines," Journal of Propulsion and Power, Vol. 22, No. 5, 2006, pp.1049-1058. crossref(new window)

Ferrier, S. D. M., Scherrer, D., Serre, L., Paridaens, C., Hendrick, P., Ingeito, A., and Bruno, C., "LAPCAT-II: conceptual design of a Mach 8 TBCC civil aircraft, enforced by full Navier-Stokes 3D nose-to-tail computation," 2011, AIAA 2011-2317

Miyagi, H., Kimura, H., and Kishi, K., "Combined Cycle Engine Research in Japanese HYPR Program," 1998, AIAA-98-3278

Chen, M., Tang, H. L., Zhu, Z. L., Ou-Yang, H., and Zhang, J., "Inlet/TBCC /Nozzle Integration Concept Design," 2008, AIAA 2008-4588

Li, C., Xu, J., Mo, J., and Zhang, K., "Numerical Study of the Unsteady Mode Transition Precess of an Over-Under TBCC Exhaust System," 2009, AIAA 2009-5301

Mo, J., Xu, J., Zhang, L., and Zhang, K., "The Experimental and Numerical Study of the Over-Under TBCC Exhaust System," 2011, AIAA 2011-2234

Slater, J. W., and Saunders, J. D., "CFD Simulation of Hypersonic TBCC Inlet Mode Transition," 2009, AIAA 2009-7349

Rolls-Royce, "The Jet Engine 5th ed.," 1996, pp.37-43.

Khan, A. N., "Computer Simuation of Turbojet-Ramjet Combination Engine," Master Thesis, Michigan State University, 1998, USA