Fluorescence imaging of mixing flowfields and comparisons with computational fluid dynamic simulations

Shock Waves

Volumn 12, Issue 2, 2002, Pages 99-110

  Gaston, M J ^a   Houwing, A F P ^b   Mudford, N R ^c   Danehy, P M ^d   Fox, J S ^b  

^a UNIVERSITY OF TECHNOLOGY SYDNEY   (Australia)

^b AUSTRALIAN NATIONAL UNIVERSITY   (Australia)

^c UNIVERSITY OF NEW SOUTH WALES   (Australia)

^d NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

Computational flow imaging; Computational fluid dynamics; Hypermixing; Planar laser induced fluorescence; Scramjet

Indexed keywords

EID: 0036706762     PISSN: 09381287     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00193-002-0151-4     Document Type: Article

References (18)

1. Baurle RA, Mathur T, Gruber MR, Jackson KR (1998) A Numerical and Experimental Investigation of a Scramjet Combustor for Hypersonic Missile Applications, AIAA Paper 98-3121, July 1998
2. Ben-Yakar A, Hanson RK (1998) Cavity Flameholders for Ignition and Flame Stabilization in Scramjets: Review and Experimental Study, AIAA paper 98-3122, July 1998
3. Boyce RR, Morton JW, Houwing AFP, Mundt C, Bone DJ (1996) Computational Fluid Dynamics Validation using Multiple Interferometric Views of a Hypersonic Flowfield, Journal of Spacecraft and Rockets 33(3): 319-325
4. CFD-ACE™, CFD Research Corporation 215 Wynn Drive Huntsville, AL 35805, USA, http://www.cfdrc.com, 2001
5. Danehy PM, Palma PC, Boyce RR, Houwing AFP (1999) Numerical Simulation of Laser-Induced Fluorescence Imaging in Shock-Layer Flows, AIAA Journal 37(6): 715-722
6. Dimotakis PE (1986), Two-dimensional shear-layer entrainment, AIAA Journal 24(11): 1791-6
7. DiRosa MD (1996) High-resolution line shape spectroscopy of transitions in the gamma bands of nitric oxide, Ph.D. Thesis, Department of Mechanical Engineering, Stanford University
8. Eklund D, Stouffer S (1994) A Numerical and Experimental Study of a Supersonic Combustor Employing Swept Ramp Injectors. AIAA/ASME/SAE/ASEE 30th Joint Propulsion Conference, Indianapolis, IN
9. Fox JS, Houwing AFP, Danehy PM, Gaston MJ, Mudford NR, Gai SL (2001) Mole-Fraction-Sensitive Imaging of Hypermixing Shear Layers, Journal of Propulsion and Power 17(2): 284-292
10. Gaston MJ, Mudford NR, Houwing AFP, Gai SL (1997) Hypermixing fuel injectors in a supersonic combustor, Proceedings of the 21st International Symposium on Shock Waves, Great Keppel Island Australia, July 1997:1113-1118
11. Gross KP, McKenzie RL, Logan P (1987) Measurements of temperature, density, pressure, and their fluctuations in supersonic turbulence using laser-induced fluorescence, Expt in Fluids 5(6): 372-380
12. Gruber MR, Baurle RA, Mathur T, Hsu KY (2001) Fundamental Studies of Cavity-based Flameholder Concepts in Supersonic Combusters, Journal of Propulson and Power 17(1): 146-153
13. O'Byrne S, Danehy PM, Gai SL, Mudford NR, Houwing AFP (1998) PLIF imaging of the separated region behind a cone in a hypersonic flow, 21st Congress of the International Council of the Aeronautical Sciences Paper ICAS-98-3.10.4, Melbourne, Australia
14. Papamosehou D, Roshko A (1988) The compressible turbulent shear layer: an experimental study, Journal of Fluid Mechanics, 197:453-77
15. +, AIAA Journal 32(8): 218-221
16. Ruyten WM, Williams WD, Heltsley FL (1994) Computational flow imaging for planar laser-induced fluorescence applications CFI-PLIF, AIAA Paper, 94-2621, 18th Aerospace Ground Testing Conference, June 1994
17. Tanner M (1984) Steady Base Flows, Progress in Aerospace Sciences, 21:81-157
18. Vincenti WG, Kruger CH (1965) Introduction to Physical Gas Dynamics, John Wiley, New York, Ch IV, p 134