1 |
Fric, T. F. and Roshko, A., "Vortical Structurein the Wake of a Transverse Jet", Journal of FluidMechanics, Vol. 279, 1994, pp. 1-47.
DOI
ScienceOn
|
2 |
Papamoschou, D. and Hubbard, D. G., "VisualObservations of Supersonic Transverse Jets",Experiments in Fluids, Vol. 14, No. 6, 1993, pp.468-471.
DOI
|
3 |
Gruber, M. R., Nejad, A. S., Chen, T. H., andDutton, J. C., "Bow Shock/Jet Interaction inCompressible Transverse Injection Flowfields",AIAA Journal, Vol. 34, No. 10, 1996, pp. 2191- 2193.
DOI
ScienceOn
|
4 |
Ben-Yakar, A., Mungal, M. G., and Hanson,R. K., "Time Evolution and Mixing Characteristicsof Hydrogen and Ethylene Transverse Jets inSupersonic Crossflows", Physics of Fluids, Vol. 18,2006. 026101.
DOI
ScienceOn
|
5 |
Peterson, D. M., Subbareddy, P. K., andCandler, G. V., "DES Investigation of TransverseInjection into Supersonic Crossflow using a HybridUnstructured Solver", AIAA Paper 2006- 903, 2006.
|
6 |
Kawai, S. and Lele, S. K., "Mechanisms of JetMixing in a Supersonic Crossflow: A Study usingLarge-Eddy Simulation", Annual Research Briefs 2007,Center for Turbulence Research, Stanford Universityand NASA-Ames, 2007, pp. 353-365.
|
7 |
Boles, J. A., Edwards, J. R., and Baurle, R.A., "Hybrid LES/RANS Simulation of TransverseSonic Injection into a Mach 2 Flow", AIAA Paper2008-622, 2008.
|
8 |
Menter, F. R., “Two-Equation Eddy-ViscosityTurbulence Models for Engineering Applications",AIAA Journal, Vol. 32, No. 8, 1994, pp.1598-1605.
DOI
ScienceOn
|
9 |
Candler, G. V., Wright, M. J., and McDonald,J. D., "Data-Parallel Lower-Upper Relaxation Methodfor Reacting Flows", AIAA Journal, Vol. 32, No.12, 1994, pp. 2380-2386.
DOI
ScienceOn
|
10 |
Wright, M. J., Candler, G. V., andPrampolini, M., "Data-Parallel Lower-UpperRelaxation Method for the Navier-StokesEquations", AIAA Journal, Vol. 34, No. 7, 1996,pp. 1371-1377.
DOI
ScienceOn
|
11 |
Wissink, A. M., Lyrintzis, A. S., andStrawn, R. C., "Parallelization of a Three-Dimensional Flow Solver for Euler RotorcraftAerodynamics Predictions", AIAA Journal, Vol. 34,No. 11, 1996, pp. 2276-2283.
DOI
ScienceOn
|
12 |
Roache, P, J., "Verification of Code andCalculations", AIAA Journal, Vol. 36, No. 5, 1998,pp. 696-702.
DOI
ScienceOn
|
13 |
원수희, 정인석, 최정열, “GCI를 이용한 수직분사제트 수치모사의 검증 및 확인", 한국항공우주학회지, 제34권, 제4호, 2006, pp. 53-63.
|
14 |
Gruber, M. R., Nejad, A. S., Chen, T. H.,and Dutton, J. C., "Mixing and PenetrationStudies of Sonic Jets in a Mach 2 Freestream",Journal of Propulsion and Power, Vol. 11, No. 2,1995, pp. 315-323.
DOI
ScienceOn
|
15 |
Yuan, L. L., Street, R. L., and Ferziger, J.H., "Large-eddy Simulation of a Round Jet inCorssflow", Journal of Fluid Mechanics, Vol. 379,1999, pp. 71-104.
DOI
ScienceOn
|
16 |
Rothstein, A. D. and Wantuck, P. J., "AStudy of the Normal Injection of Hydrogen Intoa Heated Supersonic Flow Using Planar Laser-Induced Fluorescence", AIAA Paper 92-3423, 1992.
|
17 |
Sparlat, P. R., Jou, W.-H., Strelets, M., andAllmaras, S. R., "Comments on the Feasibility ofLES for Wings, and on a Hybrid RANS/LESApproach," Advances in DNS/LES : Direct NumericalSimulation and Large Eddy Simulation, 1997, pp.137-148.
|
18 |
Strelets, M., "Detached Eddy Simulation ofMassively Separated Flows", AIAA Paper 2001-0879, 2001.
|
19 |
Kelso R. M., Lim, T. T., and Perry, A. E., "An Experimental Study of Round Jets in Corss-o rlow", Journal of Fluid Mechanics, Vol. 306, 1996, pp. 111-144.
DOI
|