Research on Transient Characteristics of Scramjet Engine during Starting Sequence
Author:
Affiliation:
1. 連絡先著者（Corresponding author）：kota.kubosaki.q7@dc.tohoku.ac.jp
2. 国立研究開発法人宇宙航空研究開発機構
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
General Medicine
Link
https://www.jstage.jst.go.jp/article/jjsass/71/1/71_71_12/_pdf
Reference26 articles.
1. 1) Tomioka, S., Tani, K., Masumoto, R. and Ueda, S.: Dual-Mode Operation of a Rocket-Ramjet Combined Cycle Engine, Trans. JSASS Aerospace Technology Japan, 8, ists27 (2010), pp. Pa_13-Pa_18.
2. 2) Davis, M. C. and White, J. T.: X-43A Flight-Test-Determined Aerodynamic Force and Moment Characteristics at Mach 7.0, J. Spacecraft Rockets, 45 (2008), pp. 472-484.
3. 3) Hank, J. M., Murphy, J. S. and Mutzman, R. C.: The X-51A Scramjet Engine Flight Demonstration Program, AIAA 2008-2540, 2008.
4. 4) Mason, J. R. and Southwick, R. D.: Large Liquid Rocket Engine Transient Performance Simulation System, NASA CR-184099, 1990.
5. 5) Majumdar, A. K., Leclair, A. C., Moore, R. and Schallhorn, P. A.: Generalized Fluid System Simulation Program, Version 6.0, NASA TM-2013-217492, 2013.
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