참고문헌 (33)

1. Meas Sci Technol D Baccarella 27 045902 2016 10.1088/0957-0233/27/4/045902 Baccarella D, Liu Q, Passaro A, Lee T, Do H (2016) Development and testing of the ACT-1 experimental facility for hypersonic combustion research. Meas Sci Technol 27:045902. https://doi.org/10.1088/0957-0233/27/4/045902 

   상세보기

2. J Propuls Power FG Billig 16 465 2000 10.2514/2.5591 Billig FG, Kothari AP (2000) Streamline tracing: technique for designing hypersonic vehicles. J Propuls Power 16:465-471. https://doi.org/10.2514/2.5591 

   상세보기

3. 10.2514/6.2016-1115 Bisek NJ (2016a) High-fidelity simulations of the HIFiRE-6 flow path. AIAA Paper 2016-1115. https://doi.org/10.2514/6.2016-1115 

   

4. 10.2514/6.2016-4276 Bisek NJ (2016b) High-fidelity simulations of the HIFiRE-6 flow path at angle of attack. AIAA Paper 2016-4276. https://doi.org/10.2514/6.2016-4276 

   

5. 10.2514/6.2006-5035 Bulman MJ, Siebenhaar A (2006) The rebirth of round hypersonic propulsion. AIAA Paper 2006-5035. https://doi.org/10.2514/6.2006-5035 

   

6. Busemann A (1942) Conical supersonic flow with axial symmetry, R.T.P. Translation No. 1598, British Ministry of Aircraft Production (from Luftfahrtforschung, 19:137-144) 

7. Exp Fluids H Do 50 1651 2011 10.1007/s00348-010-1028-4 Do H, Im S, Mungal MG, Cappelli MA (2011a) Visualizing supersonic inlet duct unstart using planar laser Rayleigh scattering. Exp Fluids 50:1651-1657. https://doi.org/10.1007/s00348-010-1028-4 

   상세보기

8. Exp Fluids H Do 51 679 2011 10.1007/s00348-011-1077-3 Do H, Im S, Mungal MG, Cappelli MA (2011b) The influence of boundary layers on supersonic inlet flow unstart induced by mass injection. Exp Fluids 51:679-691. https://doi.org/10.1007/s00348-011-1077-3 

   상세보기

9. 10.2514/6.2006-4510 Donde P, Marathe AG, Sudhakar K (2006) Starting in hypersonic intakes. AIAA Paper 2006-4510. https://doi.org/10.2514/6.2006-4510 

   

10. 10.2514/6.2006-297 Drayna TW, Nompells I, Candler GV (2006) Hypersonic inward turning inlets: design and optimization. AIAA Paper 2006-297. https://doi.org/10.2514/6.2006-297 

    

11. 10.2514/6.2015-3628 Flock AK, Riehmer JC, Gulhan A (2015) Axisymmetric scramjet engine design and performance analysis. AIAA Paper 2015-3628. https://doi.org/10.2514/6.2015-3628 

    

12. J Propuls Power J Haberle 24 446 2008 10.2514/1.33545 Haberle J, Gulhan A (2008) Investigation of two-dimensional scramjet inlet flow field at Mach 7. J Propuls Power 24:446-459. https://doi.org/10.2514/1.33545 

    상세보기

13. J Phys D Appl Phys S Im 45 485202 2012 10.1088/0022-3727/45/48/485202 Im S, Do H, Cappelli MA (2012) The manipulation of an unstarting supersonic flow by plasma actuator. J Phys D Appl Phys 45:485202. https://doi.org/10.1088/0022-3727/45/48/485202 

    상세보기

14. J Fluid Mech S Im 797 604 2016 10.1017/jfm.2016.282 Im S, Baccarella D, McGann B, Liu Q, Wermer L, Do H (2016) Unstart phenomena induced by mass addition and heat release in a model scramjet. J Fluid Mech 797:604-629. https://doi.org/10.1017/jfm.2016.282 

    상세보기

15. AIAA J FJ Malo-Molina 48 572 2010 10.2514/1.43646 Malo-Molina FJ, Gaitonde DV, Ebrahimi HB, Ruffin SM (2010) Three-dimensional analysis of a supersonic combustor coupled to innovative inward-turning inlets. AIAA J 48:572-582. https://doi.org/10.2514/1.43646 

    상세보기

16. Annu Rev Fluid Mech RB Miles 29 285 1997 10.1146/annurev.fluid.29.1.285 Miles RB, Lempert WR (1997) Quantitative flow visualization in unseeded flows. Annu Rev Fluid Mech 29:285-326. https://doi.org/10.1146/annurev.fluid.29.1.285 

    상세보기

17. J Propuls Power VS Milinda 25 555 2009 10.2514/1.37946 Milinda VS, Smart MK (2009) Shock-tunnel experiments with a Mach 12 rectangular-to-elliptical shape-transition scramjet at offdesign conditions. J Propuls Power 25:555-564. https://doi.org/10.2514/1.37946 

    상세보기

18. AIAA J S Molder 5 1252 1967 10.2514/3.4179 Molder S (1967) Internal, axisymmetric, conical flow. AIAA J 5:1252-1255. https://doi.org/10.2514/3.4179 

    상세보기

19. J Spacecr Rockets S Molder 3 1172 1966 10.2514/3.28623 Molder S, Szpiro EJ (1966) Busemann inlet for hypersonic speeds. J Spacecr Rockets 3:1172-1176. https://doi.org/10.2514/3.28649 

    상세보기

20. 10.2514/4.866609 Murthy SNB, Curran ET (2001) Scramjet propulsion. Progress in astronautics and aeronautics, vol 189, pp 447-511. https://doi.org/10.2514/4.866609 

    

21. J Propuls Power H Ogawa 26 1247 2010 10.2514/1.48284 Ogawa H, Grainer AL, Boyce RR (2010) Inlet starting of high-contraction axisymmetric scramjet. J Propuls Power 26:1247-1258. https://doi.org/10.2514/1.48284 

    상세보기

22. J Propuls Power SE Otto 32 1178 2016 10.2514/1.B36028 Otto SE, Trefny CJ, Slater JW (2016) Inward-turning streamline-traced inlet design method for low-boom, low-drag applications. J Propuls Power 32:1178-1189. https://doi.org/10.2514/1.B36028 

    상세보기

23. Exp Fluids J Poggie 37 438 2004 10.1007/s00348-004-0828-9 Poggie J, Erbland PJ, Smits AJ, Miles RB (2004) Quantitative visualization of compressible turbulent shear flows using condensate-enhanced Rayleigh scattering. Exp Fluids 37:438-454. https://doi.org/10.1007/s00348-004-0828-9 

    상세보기

24. J Propuls Power BU Reinartz 19 868 2003 10.2514/2.6177 Reinartz BU, Herrmann CD, Ballmann J, Koshel WW (2003) Aerodynamic performance analysis of a hypersonic inlet isolator using computation and experiment. J Propuls Power 19:868-875. https://doi.org/10.2514/2.6177 

    상세보기

25. 10.2514/6.2014-3593 Slater JW (2014) Methodology for the design of streamline-traced external-compression supersonic inlets. AIAA Paper 2014-3593. https://doi.org/10.2514/6.2014-3593 

    

26. J Aircr MK Smart 36 430 1999 10.2514/2.2448 Smart MK (1999a) Optimization of two-dimensional scramjet inlets. J Aircr 36:430-433. https://doi.org/10.2514/2.2448 

    상세보기

27. J Propuls Power MK Smart 15 408 1999 10.2514/2.5459 Smart MK (1999b) Design of three-dimensional hypersonic inlets with rectangular-to-elliptical shape transition. J Propuls Power 15:408-416. https://doi.org/10.2514/2.5459 

    상세보기

28. J Propuls Power MK Smart 17 276 2001 10.2514/2.5774 Smart MK (2001) Experimental testing of a hypersonic inlet with rectangular-to-elliptical shape transition. J Propuls Power 17:276-283. https://doi.org/10.2514/2.5774 

    상세보기

29. Aeronaut J MK Smart 111 605 2007 10.1017/S0001924000004796 Smart MK (2007) Scramjets. Aeronaut J 111:605-619. https://doi.org/10.1017/S0001924000004796 

    상세보기

30. AIAA J MK Smart 50 610 2012 10.2514/1.J051281 Smart MK (2012) How much compression should a scramjet inlet do? AIAA J 50:610-619. https://doi.org/10.2514/1.J051281 

    상세보기

31. 10.2514/6.1996-2914 Van Wie DM, Kwok FT, Walsh RF (1996) Starting characteristics of supersonic inlets. AIAA Paper 1996-2914. https://doi.org/10.2514/6.1996-2914 

    

32. AIAA J JL Wagner 47 1528 2009 10.2514/1.40966 Wagner JL, Yuceil KB, Valdivia A, Clemens NT, Dolling DS (2009) Experimental investigation of unstart in an inlet/isolator model in Mach 5 flow. AIAA J 47:1528-1542. https://doi.org/10.2514/1.40966 

    상세보기

33. AIAA J P Wu 38 672 2000 10.2514/2.1009 Wu P, Lempert WR, Miles RB (2000) Megahertz pulse-burst laser and visualization of shockwave/boundary-layer interactions. AIAA J 38:672-679. https://doi.org/10.2514/2.1009 

    상세보기

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