Advances in aircraft and spacecraft science

  • 제5권4호
  • /
  • Pages.431-444
  • /
  • 2018
  • /
  • 2287-528X(pISSN)
  • /
  • 2287-5271(eISSN)
테크노프레스 (Techno-Press)
권호 표지
DOI QR코드

DOI QR Code

Effect of control route on the unstart/restart characteristics of an over-under TBCC inlet

  • Li, Nan (Science and Technology on Scramjet Laboratory, Hypervelocity Aerodynamics Institute of CARDC) ;
  • Chang, Juntao (Harbin Institute of Technology) ;
  • Tang, Jingfeng (Harbin Institute of Technology) ;
  • Yu, Daren (Harbin Institute of Technology) ;
  • Bao, Wen (Harbin Institute of Technology) ;
  • Song, Yanping (Harbin Institute of Technology)
  • 투고 : 2017.09.25
  • 심사 : 2017.12.27
  • 발행 : 2018.07.25
⟨ 이전 논문 다음 논문 ⟩

초록

Numerical simulations have been conducted to study the unstart/restart characteristics of an over-under turbine-based combined-cycle propulsion system (TBCC) inlet during the inlet transition phase. A dual-solution area exists according to the Kantrowitz theory, in which the inlet states may be different even with the same input parameters. The entire transition process was divided into five stages and the unstart/restart hysteresis loop for each stage was also obtained. These loops construct a hysteresis surface which separates the operating space of the engine into three parts: in which a) inlet can maintain a started state; b) inlet keeps an unstarted state; c) inlet state depends on its initial state. During the transition, the operation of the engine follows a certain order with different backpressures and splitter angles, namely control route, which may result in disparate inlet states. Nine control routes with different backpressures and transition stages were designed to illuminate the route-dependent behavior of the inlet. The control routes operating towards the unstart boundary can make the inlet transit from a started state into an unstarted one. But operating backward the same route cannot make the inlet restart, additional effort should be made.

키워드

과제정보

연구 과제 주관 기관 : National Natural Science Foundation of China

참고문헌

  1. Chang, J.T., Li, N., Xu, K.J., Bao, W. and Yu, D.R. (2017), "Recent research progress on unstart mechanism, detection and control of hypersonic inlet", Prog. Aerosp. Sci., 89, 1-22. https://doi.org/10.1016/j.paerosci.2016.12.001
  2. Chang, J.T., Bao, W., Yu, D.R. and Shen, Y. (2009), "Effects of wall cooling on performance parameters of hypersonic inlets", Acta Astron., 65(3), 467-476. https://doi.org/10.1016/j.actaastro.2009.02.005
  3. Cui, T., Lv, Z. and Yu, D.R. (2011), "Multistability and complex routes of supersonic inlet start/unstart", J. Propul. Power, 27(6), 1204-1217. https://doi.org/10.2514/1.B34235
  4. Cui, T., Tang, S.L., Zhang, C. and Yu, D.R. (2012), "Hysteresis phenomenon of mode transition in ramjet engines and its topological rule", J. Propul. Power, 28(6), 1277-1284. https://doi.org/10.2514/1.B34419
  5. Cui, T., Wang, Y. and Yu, D.R. (2014), "Bistability and hysteresis in a nonlinear dynamic model of shock motion", J. Aircraft, 51(5), 1373-1379. https://doi.org/10.2514/1.C032175
  6. Fu, C.G., Zeng, H., He, L.M., Sun, C.J. and Zhao, K. (2016), "Investigation on the influence of nozzle configuration on performance of a 2-stage PDE", Acta Aerodyn. Sin., 34(6), 770-777.
  7. Haberle, J. and Gulhan, A. (2008), "Investigation of two-dimensional scramjet inlet fowfeld at Mach 7", J. Propul. Power, 24(3), 446-459. https://doi.org/10.2514/1.33545
  8. Herrmann, C.D. and Koschel, W.W. (2002), "Experimental investigation of the internal compression of a hypersonic intake", Proceedings of the 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, U.S.A., July.
  9. Kantrowitz, A. and Donaldson, C. (1945), "Preliminary investigation of supersonic diffusers", NACA Rept. ACR-L5D20; Langley Memorial Aeronautical Laboratory, U.S.A.
  10. Kuzmin, A. (2015), "Shock Wave instability in a channel with an expansion corner", J. App. Mech., 7(2), 1-9.
  11. Kuzmin, A. (2016a), "Shock wave bifurcation in convergent-divergent channels of rectangular cross section", Shock Waves, 26(6), 741-747. https://doi.org/10.1007/s00193-016-0624-5
  12. Kuzmin, A. (2016b), "Shock wave bifurcation in channels with a bend", Arch. Appl. Mech., 86(5), 787-795. https://doi.org/10.1007/s00419-015-1062-z
  13. Luo, J.L., Zhou, D., Kang, H.L. and Wang J.K. (2014), "Summarization of experimental methods associated with typical aerodynamic issues", Acta Aerodyn. Sin., 32(5), 600-609.
  14. Menter, F.R. (1994), "Two-equation eddy-viscosity turbulence models for engineering applications", AIAA J., 32(8), 1598-1605. https://doi.org/10.2514/3.12149
  15. Norris, G. (2011), "X-51A scramjet fails on second attempt", Aerosp. Daily Defense Rep., 238(55).
  16. Raj, N. and Venkatasubbaiah, K. (2012), "A new approach for the design of hypersonic scramjet inlets", Phys. Fluids, 24(8), 86103. https://doi.org/10.1063/1.4748130
  17. Saunders, J.D., Slater, J.W., Dippold, V., Lee, J., Sanders, B.W. and Weir, L.J. (2008), "Inlet mode transition screening test for a turbine-based combined-cycle propulsion system", Joint Army-Navy-NASA-Air Force, Boston, U.S.A., May.
  18. Taha, A.A., Tiwari, S.N. and Mohieldin, T.O. (2001), "Validation of fluent CFD code in supersonic flow fields", Proceedings of the 15th AIAA Computational Fluid Dynamics Conference, Fluid Dynamics and Co-located Conferences, Anaheim, U.S.A., June.
  19. Voland, R.T. and Auslender, A.H. (1999), "CIAM/NASA Mach 6.5 scramjet flight and ground test", Proceedings of the 9th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Norfolk, U.S.A., November.
  20. Wagner, J.L., Yuceil, K.B., Valdivia, A., Clemens, N.T. and Dolling, D.S. (2009), "Experimental investigation of unstart in an inlet/isolator model in Mach 5 flow", AIAA J., 47(6), 1528-1542. https://doi.org/10.2514/1.40966
  21. Walker, S., Rodgers, F., Paull, A. and Van Wie, D.M. (2008), "HyCAUSE flight test program", Proceedings of the 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, U.S.A., April.
  22. Wang, D.P., Zhuang, Y., Tan, H.J., Zhang, H., Du, M.C. and Li, G.S. (2011), "Design and simulation of a dual-channel variable geometry turbine based combined inlet", J. Aero. Power, 11(30), 2695-2704.
  23. Wilcox, D.C. (1994), Turbulence modeling for CFD, DCW Industries, CA, U.S.A.
  24. Zhao, H.Y. and Yi, M.R. (2014), "Review of design for forced-transition trip of hypersonic inlet", Acta Aerodyn. Sin., 32(5), 623-627.