참고문헌 (35)

1. 10.2514/6.2013-1130 Grossir G, Paris S, Bensassi K, Rambaud P (2013) Experimental characterization of hypersonic nozzle boundary layers and free-stream noise levels. In: 51st AIAA Aerosp Sci Meet Incl New Horizons Forum Aerosp Expo, AIAA Paper 2013-1130, Grapevine, Texas 

   

2. Pate SR (1978) Dominance of radiated aerodynamic noise on boundary-layer transition in supersonic-hypersonic wind tunnels theory and application. In: NASA Technical Report, AEDC-TR-77-107 

3. 10.21236/ADA384962 Pate SR (1980) Effects of wind tunnel disturbances on boundary-layer transition with emphasis on radiated noise: a review. In: 11th Aerodynamic Testing Conf, Colorado 

   

4. Harvey WD (1978) Influence of free-stream disturbances on boundary-layer transition. In: NASA Technical Memorandum, NASA TM-78635 

5. Sivells JC (1978) A computer program for the aerodynamic design of axisymmetric and planar nozzles for supersonic and hypersonic wind tunnels. In: NASA Technical Report, AEDC-TR-78-63 

6. 10.2514/6.1969-337 Sivells JC (1969) Aerodynamic design of axisymmetric hypersonic wind tunnel nozzles. In: 4th Aerodynamic Testing Conf, AIAA Paper 1969-337, Arnold Air Force Station, Tennessee 

   

7. 10.2514/6.2006-3665 Shope F (2006) Contour design techniques for super/hypersonic wind tunnel nozzles. In: 24th AIAA Applied Aerodynamics Conference, AIAA Paper 2006-3665, San Francisco, California 

   

8. J Propuls Power WYK Chan 34 6 1467 2018 10.2514/1.B36938 Chan WYK, Jacobs PA, Smart MK, Grieve S, Craddock CS, Doherty LJ (2018) Aerodynamic design of nozzles with uniform outflow for hypervelocity ground-test facilities. J Propuls Power 34(6):1467-1478. https://doi.org/10.2514/1.B36938 

   상세보기

9. Benton J, Perkins J, Edwards A (1990) Limitations of the method of characteristics when applied to axisymmetric hypersonic nozzle design. In: 28th Aerosp Sci Meeting, In: AIAA Paper 1990-192, Reno, Nevada 

10. 10.2514/6.1991-297 Candler G, Perkins J (1991) Effects of vibrational nonequilibrium on axisymmetric hypersonic nozzle design. In: 29th Aerosp Sci Meeting, AIAA Paper 1991-297, Reno, Nevada 

    

11. 10.1063/1.5065334 Akinin SA, Goldfeld MA, Starov AV (2018) Flow parameters at the supersonic combustor entrance at tests in quasistationary impulse regime. In: Int Conf on the Methods of Aerophysical Research, Novosibirsk, Russia 

    

12. J Fluids Eng J Mi 123 4 878 2001 10.1115/1.1412460 Mi J, Nathan GJ, Nobes DS (2001) Mixing characteristics of axisymmetric free jets from a contoured nozzle, an orifice plate and a pipe. J Fluids Eng 123(4):878-883. https://doi.org/10.1115/1.1412460 

    상세보기

13. Eur J Mech B/Fluids WR Quinn 25 3 279 2006 10.1016/j.euromechflu.2005.10.002 Quinn WR (2006) Upstream nozzle shaping effects on near field flow in round turbulent free jets. Eur J Mech B/Fluids 25(3):279-301. https://doi.org/10.1016/j.euromechflu.2005.10.002 

    상세보기

14. Yang SM (2019) Force and moment measurement of supersonic free-flight models in Konkuk University Ludwieg tube. Master Thesis, Konkuk University 

15. J Korean Soc Aeronaut Sp Sci YJ Kim 46 9 703 2018 10.5139/JKSAS.2018.46.9.703 Kim YJ, Byun YH, Park SH, Park G, Lee J (2018) Concept design of Ludwieg tube at Konkuk University. J Korean Soc Aeronaut Sp Sci 46(9):703-711. https://doi.org/10.5139/JKSAS.2018.46.9.703 

    원문보기 상세보기

16. J Spacecr Rockets FFJ Schrijer 47 1 125 2010 10.2514/1.40773 Schrijer FFJ, Bannink WJ (2010) Description and flow assessment of the Delft hypersonic Ludwieg tube. J Spacecr Rockets 47(1):125-133. https://doi.org/10.2514/1.40773 

    상세보기

17. HW Liepmann 2001 Elements of gasdynamics Liepmann HW, Roshko A (2001) Elements of gasdynamics. Dover, New York 

18. Oosthuizen PH, Carscallen WE (1997) Variable area flow. In: Compressible fluid flow. McGraw-Hill, International Ed, pp 174-224 

19. J Propuls Power S Leonov 34 2 499 2018 10.2514/1.B36811 Leonov S, Houpt A, Elliott S, Hedlund B (2018) Ethylene ignition and flameholding by electrical discharge in supersonic combustor. J Propuls Power 34(2):499-509. https://doi.org/10.2514/1.B36811 

    상세보기

20. Acta Astronaut J Tan 144 30 2018 10.1016/j.actaastro.2017.12.010 Tan J, Zhang D, Li H, Hou J (2018) Detailed experimental investigations on flow behaviors and velocity field properties of a supersonic mixing layer. Acta Astronaut 144:30-38. https://doi.org/10.1016/j.actaastro.2017.12.010 

    상세보기

21. Therm Sci PK Mohanta 21 6B 3001 2017 10.2298/TSCI151224214M Mohanta PK, Sridhar BTN (2017) Study of decay characteristics of rectangular and elliptical supersonic jets. Therm Sci 21(6B):3001-3010. https://doi.org/10.2298/TSCI151224214M 

    상세보기

22. Exp Fluids A Houpt 58 4 25 2017 10.1007/s00348-016-2295-5 Houpt A, Hedlund B, Leonov S, Ombrello T, Carter C (2017) Quasi-DC electrical discharge characterization in a supersonic flow. Exp Fluids 58(4):25. https://doi.org/10.1007/s00348-016-2295-5 

    상세보기

23. Int J Aeronaut Sp Sci I Kim 18 3 425 2017 10.5139/IJASS.2017.18.3.425 Kim I, Lee S, Park G, Lee JK (2017) Overview of flow diagnosis in a shock tunnel. Int J Aeronaut Sp Sci 18(3):425-435. https://doi.org/10.5139/IJASS.2017.18.3.425 

    원문보기 상세보기

24. 10.2514/6.2017-2155 Wang Q, Li JW, Lu P, Li JP, Zhao W, Jiang ZL (2017) Pressure and heat flux calibration of the long-test-duration hypervelocity detonation-driven shock tunnel. In: 21st AIAA International Space Planes and Hypersonics Technologies Conference, AIAA Paper 2017-2155, Xiamen, China 

    

25. Acta Astronaut K Kim 161 446 2019 10.1016/j.actaastro.2019.02.022 Kim K, Park G, Jin S (2019) Flameholding characteristics of ethylene-fueled model scramjet in shock tunnel. Acta Astronaut 161:446-464. https://doi.org/10.1016/j.actaastro.2019.02.022 

    상세보기

26. AIAA J S Lee 55 11 3995 2017 10.2514/1.J055967 Lee S, Song H, Park G, Lee JK (2017) Freefalling heated sphere in a shock tunnel. AIAA J 55(11):3995-3998. https://doi.org/10.2514/1.J055967 

    상세보기

27. J Propuls Power WK Chang 32 5 1230 2016 10.2514/1.B36007 Chang WK, Park G, Jin Y, Byun J (2016) Shock impinging effect on ethylene flameholding. J Propuls Power 32(5):1230-1239. https://doi.org/10.2514/1.B36007 

    상세보기

28. Aerosp Sci Technol EWK Chang 80 413 2018 10.1016/j.ast.2018.07.012 Chang EWK, Yang S, Park G, Choi H (2018) Ethylene flame-holding in double ramp flows. Aerosp Sci Technol 80:413-423. https://doi.org/10.1016/j.ast.2018.07.012 

    상세보기

29. ANSYS Inc (2013) Introduction to ANSYS Fluent. ANSYS Inc, Canonsburg, PA 

30. ANSYS Inc (2013) Ansys Fluent user’s guide. ANSYS Inc, Canonsburg, PA 

31. Oliden D (2013) Parametric analysis of a hypersonic inlet using computational fluid dynamics. Master Thesis, Arizona State University 

32. J Phys Chem Ref Data K Kadoya 14 4 947 1985 10.1063/1.555744 Kadoya K, Matsunaga N, Nagashima A (1985) Viscosity and thermal conductivity of dry air in the gaseous phase. J Phys Chem Ref Data 14(4):947-970. https://doi.org/10.1063/1.555744 

    상세보기

33. 10.2514/6.2005-4424 Rodriguez CG, Cutler AD (2005) Computational simulation of a supersonic-combustion benchmark experiment. In: 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA Paper 2005-4424, Tucson, Arizona 

    

34. J Spacecr Rockets EDV Bigarella 44 1 52 2007 10.2514/1.23843 Bigarella EDV, Azevedo JLF, Scalabrin LC (2007) Centered and upwind multigrid turbulent flow simulations of launch vehicle configurations. J Spacecr Rockets 44(1):52-65. https://doi.org/10.2514/1.23843 

    상세보기

35. Carlson DR, Walters WP (1966) A supersonic/hypersonic aerodynamic investigation of the Saturn IB/Apollo upper stage. In: NASA Contract Report, NASA CR-362 

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