$\require{mediawiki-texvc}$

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

[해외논문] Visualization of streamline tracing inlet-isolator flows using a planar laser Rayleigh scattering imaging technique

Journal of visualization, v.22 no.2, 2019년, pp.359 - 369  

DiCristina, Giovanni ,  Kang, Kyungrae ,  Song, Seung Jin ,  Choi, Jong Ho ,  Do, Hyungrok ,  Im, Seong-kyun

초록이 없습니다.

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 crossref

  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 crossref

  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 

    crossref

  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 

    crossref

  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 

    crossref

  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 crossref

  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 crossref

  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 

    crossref

  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 

    crossref

  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 

    crossref

  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 crossref

  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 crossref

  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 crossref

  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 crossref

  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 crossref

  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 crossref

  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 crossref

  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 crossref

  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 

    crossref

  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 crossref

  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 crossref

  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 crossref

  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 crossref

  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 

    crossref

  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 crossref

  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 crossref

  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 crossref

  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 crossref

  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 crossref

  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 

    crossref

  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 crossref

  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 crossref
LOADING...

관련 콘텐츠

이 논문과 함께 이용한 콘텐츠

유발과제정보 저작권 관리 안내
섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트

맨위로