Transverse jet injection into a supersonic turbulent cross-flow

Physics of Fluids

Volumn 23, Issue 4, 2011, Pages

  Rana, Z A ^a   Thornber, B ^a   Drikakis, D ^a  

^a CRANFIELD UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; COMBUSTION CHAMBERS; COMPUTATIONAL FLUID DYNAMICS; DIGITAL FILTERS; KINETIC ENERGY; KINETICS; LARGE EDDY SIMULATION; MIXING; NUMERICAL METHODS; REYNOLDS NUMBER; ROCKETS; RUNGE KUTTA METHODS; SUPERSONIC AERODYNAMICS; TURBULENT FLOW; VECTOR CONTROL (ELECTRIC MACHINERY); VORTEX FLOW;

COMPUTATIONAL RESOURCES; IMPLICIT LARGE EDDY SIMULATIONS; RUNGE-KUTTA SCHEMES; SCRAMJET COMBUSTION CHAMBER; STRONG STABILITY PRESERVING; SUPERSONIC CROSS FLOW; SUPERSONIC TURBULENT BOUNDARY LAYERS; TURBULENT KINETIC ENERGY;

FIGHTER AIRCRAFT;

EID: 79955456510     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.3570692     Document Type: Article

References (66)

1. Humble R. Henry G. Larson W. Space Propulsion Analysis and Design 1995, and 2nd ed. (McGraw-Hill, New York, ).
2. Ko H. Yoon W. Performance analysis of secondary gas injection into a conical rocket nozzle. J. Propul. Power 2002, 18:585. JPPOEL, 0748-4658, 10.2514/2.5972.
3. Sarno R. Franke M. Suppression of flow-induced pressure oscillations in cavities. J. Aircr. 1994, 31:90. JAIRAM, 0021-8669, 10.2514/3.46459.
4. Ukeiley L.S. Ponton M.K. Seiner J.M. Jansen B. Suppression of pressure loads in cavity flows. AIAA J. 2004, 42:70. AIAJAH, 0001-1452, 10.2514/1.9032.
5. Vakili A.D. Gauthier C. Control of cavity flow by upstream mass-injection. J. Aircr. 1994, 31:169. JAIRAM, 0021-8669, 10.2514/3.46470.
6. Rowley C.W. Williams D.R. Dynamics and control of high Reynolds number flow over open cavities. Annu. Rev. Fluid Mech. 2006, 38:251. ARVFA3, 0066-4189, 10.1146/annurev.fluid.38.050304.092057.
7. Cattafesta L. Williams D. Rowley C. Alvi F. Review of active control of flow induced cavity resonance. 2003, and AIAA Paper No. 2003-3567.
8. Schramm J. Karl S. Hannemann K. Steelant J. Ground testing of the Hyshot-II scramjet configuration in HEG. 2008, and 15th AIAA Space Planes and Hypersonic Systems Conference, Dayton, AIAA Paper No. 2547.
9. Davidenko D. Gokalp I. Dufour E. Magre P. Numerical simulation of hydrogen supersonic combustion and validation of computational approach. 2003, and 12th AIAA International Space Planes and Hypersonic Systems and Technologies, Virginia, AIAA Paper No. 7033.
10. Gardner A. Hannemann K. Steelant J. Paull A. Ground testing of the Hyshot supersonic combustion flight experiment in HEG and comparison with flight data. 2004, and 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Florida, AIAA Paper No. 3345.
11. Furudate M. Lee B. Jeung I. Computation of Hyshot scramjet flows in the T4 experiments. 2005, and AIAA/CIRA 13th International Space Planes and Hypersonic Systems and Technologies, AIAA Paper No. 3353.
12. Love E. Grigsby C. Some studies of symmetric free jets exhausting from sonic and supersonic nozzles into still air and into supersonic streams. 1955, and NACA Report No. RM-L54L31.
13. Billig F. Orth R. Lasky M. A unified analysis of gaseous jet penetration. AIAA J. 1971, 9:1048. AIAJAH, 0001-1452, 10.2514/3.49916.
14. Admason T. Nicholls J. On the structure of jets from highly underexpanded nozzles into still air. J. Aerosp. Sci. 1959, 26:16. JASSA7, 0095-9820.
15. Schetz J. Billig F. Penetration of gaseous jets injected into a supersonic stream. J. Spacecr. Rockets 1966, 3:1658. JSCRAG, 0022-4650, 10.2514/3.28721.
16. Cohen L. Coulter L. Egan W. Penetration and mixing of multiple gas jets subjected to a crossflow. AIAA J. 1971, 9:718. AIAJAH, 0001-1452, 10.2514/3.6253.
17. Orth R. Funk J. An experimental and comparative study of jet penetration in supersonic flow. J. Spacecr. Rockets 1967, 4:1236. JSCRAG, 0022-4650, 10.2514/3.29058.
18. Ben-Yakar A. Mungal M.G. Hanson R.K. Time evolution and mixing characteristics of hydrogen and ethylene transverse jets in supersonic crossflows. Phys. Fluids 2006, 18:026101. PHFLE6, 1070-6631, 10.1063/1.2139684.
19. Gruber M. Nejad A. Chen T. Dutton J. Mixing and penetration studies of sonic jets in a Mach 2 freestream. J. Propul. Power 1995, 11:315. JPPOEL, 0748-4658, 10.2514/3.51427.
20. Zukoski E. Spaid F. Secondary injection of gases into a supersonic flow. AIAA J. 1964, 2:1689. AIAJAH, 0001-1452, 10.2514/3.2653.
21. Calarese W. Sakell L. Zakkay V. An experimental investigation of the interaction between a transverse sonic jet and a hypersonic stream. AIAA J. 1971, 9:674. AIAJAH, 0001-1452, 10.2514/3.6247.
22. Kaufman L. Hypersonic flow past transverse jets. J. Spacecr. Rockets 1967, 4:1230. JSCRAG, 0022-4650, 10.2514/3.29057.
23. Vanierschot M. Persoons T. Van den Bulck E. A new method for annular jet control based on cross-flow injection. Phys. Fluids 2009, 21:025103. PHFLE6, 1070-6631, 10.1063/1.3037343.
24. Chauvet N. Deck S. Jacquin L. Shock patterns in a slightly underexpanded sonic jet controlled by radial injections. Phys. Fluids 2007, 19:048104. PHFLE6, 1070-6631, 10.1063/1.2720836.
25. Zong N. Meng H. Hsieh S. Yang V. A numerical study of cryogenic fluid injection and mixing under supercritical conditions. Phys. Fluids 2004, 16:4248. PHFLE6, 1070-6631, 10.1063/1.1795011.
26. Aswin G. Chakraborty D. Numerical simulation of transverse side jet interaction with supersonic free stream. Aerosp. Sci. Technol. 2010, 14:295. ARSTFZ, 1270-9638, 10.1016/j.ast.2010.02.001.
27. Santiago J. Dutton J. Velocity measurements of a jet injected into a supersonic flow. J. Propul. Power 1997, 13:264. JPPOEL, 0748-4658, 10.2514/2.5158.
28. Everett D. Woodmansee M. Dutton J. Morris M. Wall pressure measurements for a sonic jet injected transversely into a supersonic crossflow. J. Propul. Power 1998, 14:861. JPPOEL, 0748-4658, 10.2514/2.5357.
29. VanLerberghe W.M. Santiago J.G. Dutton J.C. Lucht R.P. Mixing of a sonic transverse jet injected into a supersonic flow. AIAA J. 2000, 38:470. AIAJAH, 0001-1452, 10.2514/2.984.
30. Génin F. Menon S. Dynamics of sonic jet injection into supersonic crossflow. J. Turbul. 2010, 11:4. ZZZZZZ, 1468-5248, 10.1080/14685240903217813.
31. Kawai S. Lele S. Large-eddy simulation of jet mixing in a supersonic turbulent crossflow. 2009, and 19th AIAA Computational Fluid Dynamics, San Antonio, Texas, AIAA Paper No. 2009-3795, June.
32. Kawai S. Lele S. Large-eddy simulation of jet mixing in supersonic turbulent crossflows. AIAA J. 2010, 48:2063. AIAJAH, 0001-1452, 10.2514/1.J050282.
33. Klein M. Sadiki A. Janicka J. A digital filter based generation of inflow data for spatially developing direct numerical or large eddy simulations. J. Comput. Phys. 2003, 186:652. JCTPAH, 0021-9991, 10.1016/S0021-9991(03)00090-1.
34. Thornber B. Drikakis D. Williams R. Youngs D. On entropy generation and dissipation of kinetic energy in high-resolution shock-capturing schemes. J. Comput. Phys. 2008, 227:4853. JCTPAH, 0021-9991, 10.1016/j.jcp.2008.01.035.
35. Spiteri R. Ruuth S. A new class of optimal high-order strong-stability-preserving time discretization method. SIAM (Soc. Ind. Appl. Math.) J. Numer. Anal. 2002, 40:469. SJNAAM, 0036-1429, 10.1137/S0036142901389025.
36. Xie Z. Castro I. Efficient generation of inflow conditions for large eddy simulation of street-scale flows. Flow, Turbul. Combust. 2008, 81:449. FTCOF9, 1386-6184, 10.1007/s10494-008-9151-5.
37. Touber E. Sandham N. Large-eddy simulation of low-frequency unsteadiness in a turbulent shock-induced separation bubble. Theor. Comput. Fluid Dyn. 2009, 23:79. TCFDEP, 0935-4964, 10.1007/s00162-009-0103-z.
38. Drikakis D. Advances in turbulent flow computations using high-resolution methods. Prog. Aerosp. Sci. 2003, 39:405. PAESD6, 0376-0421, 10.1016/S0376-0421(03)00075-7.
39. Drikakis D. Tsangaris S. Real gas effects for compressible nozzle flow. ASME Trans. J. Fluids Eng. 1993, 115:115. JFEGA4, 0098-2202, 10.1115/1.2910092.
40. Drikakis D. Tsangaris S. On the accuracy and efficiency of CFD methods in real gas hypersonics. Int. J. Numer. Methods Fluids 1993, 16:759. IJNFDW, 0271-2091, 10.1002/fld.1650160902.
41. Zółtak J. Drikakis D. Hybrid upwind methods for the simulation of unsteady shock-wave diffraction over a cylinder. Comput. Methods Appl. Mech. Eng. 1998, 162:165. CMMECC, 0045-7825, 10.1016/S0045-7825(97)00342-3.
42. Bagabir A. Drikakis D. Numerical experiments using high-resolution schemes for unsteady, inviscid, compressible flows. Comput. Methods Appl. Mech. Eng. 2004, 193:4675. CMMECC, 0045-7825, 10.1016/j.cma.2004.03.012.
43. Toro E. Riemann Solvers and Numerical Methods for Fluid Dynamics: A Practical Introduction 2009, 10.1007/b79761, 3rd ed. (Springer-Verlag, Berlin, ).
44. Drikakis D. Rider W. High-Resolution Methods for Incompressible and Low-Speed Flows 2005, and (Springer-Verlag, Berlin, ).
45. Rana Z. Thornber B. Drikakis D. 2009, and Large eddy simulation of a scramjet model (Hyshot-II) using high-resolution methods, 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Denver, Colorado.
46. Thornber B. Drikakis D. Large eddy simulation of a deep cavity using high-resolution methods. 2008, and 46th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper No. 0730.
47. Thornber B. Drikakis D. Williams R. Mosedale A. Youngs D. An improved reconstruction method for compressible flows with low Mach number features. J. Comput. Phys. 2008, 227:4873. JCTPAH, 0021-9991, 10.1016/j.jcp.2008.01.036.
48. Thornber B. Drikakis D. Youngs D. Williams R. The influence of initial conditions on turbulent mixing due to Richtmyer-Meshkov instability. J. Fluid Mech. 2010, 654:99. JFLSA7, 0022-1120, 10.1017/S0022112010000492.
49. Rana Z. Thornber B. Drikakis D. CFD analysis of a scramjet model using high-resolution methods. 2009, and Proceedings of European Air and Space Conference (CEAS-2009), Manchester, UK.
50. Rana Z. Drikakis D. Investigation of sonic jet mixing in a stream of supersonic cross-flow using large eddy simulations. 2010, and Proceedings of 27th Congress of the International Council of the Aeronautical Sciences (ICAS-2010), Nice, France.
51. Godunov S. A finite-difference method for the computation of discontinuous solutions of the equations of fluid dynamics. Mat. Sb. 1959, 47:271. MATSAB, 0368-8666.
52. Van Leer B. Towards the ultimate conservative difference scheme. IV. A new approach to numerical convection. J. Comput. Phys. 1977, 23:276. JCTPAH, 0021-9991, 10.1016/0021-9991(77)90095-X.
53. Kim C. Kim K.H. Accurate, efficient and monotonic numerical methods for multidimensional compressible flows. Part II. Multi-dimensional limiting process. J. Comput. Phys. 2005, 208:570. JCTPAH, 0021-9991, 10.1016/j.jcp.2005.02.022.
54. Guillard H. Murrone A. On the behaviour of upwind schemes in the low Mach number limit: II. Godunov type schemes. Comput. Fluids 2004, 33:655. CPFLBI, 0045-7930, 10.1016/j.compfluid.2003.07.001.
55. Kolomogorov A. The local structure of turbulence in an incompressible fluid at very high Reynolds numbers. Dokl. Akad. Nauk SSSR 1941, 30:299. DANKAS, 0002-3264.
56. Thornber B. Starr M. Drikakis D. Implicit large eddy simulation of ship air-wakes. Aeronaut. J. 2010, 114:99. AENJAK, 0001-9240.
57. Grinstein F. Margolin L. Rider W. Implicit Large Eddy Simulation: Computing Turbulent Fluid Dynamics 2007, 10.1017/CBO9780511618604, and (Cambridge University Press, Cambridge, ).
58. Drikakis D. Hahn M. Mosedale A. Thornber B. Large eddy simulation using high-resolution and high-order methods. Philos. Trans. R. Soc. London, Ser. A 2009, 367:2985. PTRMAD, 0962-8428, 10.1098/rsta.2008.0312.
59. Courant R. Friedrichs K. Lewy H. On the partial difference equations of mathematical physics. IBM Journal 1967, 11:215. 10.1147/rd.112.0215.
60. Lund T. Wu X. Squires K. Generation of turbulent inflow data for spatially-developing boundary layer simulations. J. Comput. Phys. 1998, 140:233. JCTPAH, 0021-9991, 10.1006/jcph.1998.5882.
61. Pirozzoli S. Grasso F. Gatski T.B. Direct numerical simulation and analysis of a spatially evolving supersonic turbulent boundary layer at M=2.25. Phys. Fluids 2004, 16:530. PHFLE6, 1070-6631, 10.1063/1.1637604.
62. Pirozzoli S. Bernardini M. Grasso F. Characterization of coherent vortical structures in a supersonic turbulent boundary layer. J. Fluid Mech. 2008, 613:205231. JFLSA7, 0022-1120, 10.1017/S0022112008003005.
63. θ=1410. J. Fluid Mech. 1988, 187:61. JFLSA7, 0022-1120, 10.1017/S0022112088000345.
64. Abramovich G. The Theory of Turbulent Jets 1963, English ed. (Massachusetts Institute of Technology Press, Cambridge, MA, ), Chap. 12, Sec. 4.
65. Viti V. Neel R. Schetz J. Detailed flow physics of the supersonic jet interaction flow field. Phys. Fluids 2009, 21:046101. PHFLE6, 1070-6631, 10.1063/1.3112736.
66. Thornber B. Drikakis D. Implicit large-eddy simulation of a deep cavity using high-resolution methods. AIAA J. 2008, 46:2634. AIAJAH, 0001-1452, 10.2514/1.36856.