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VULCAN RELATED PUBLICATIONS
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Hypersonic Airbreathing Propulsion Branch
Hypersonic Airbreathing Propulsion Branch


The following is a list of VULCAN related publications :
  1. Baurle, R.A., "CFD Analysis of a Rectangular-to-Elliptical Shape Transition Engine Flowpath" 41st JANNAF CS / 29th APS / 23rd PSHS Joint Meeting, San Diego, Ca, Dec 2006.
  2. Baurle, R.A., Tam, C.-J., Edwards, J.R., and Hassan, H.A., "Hybrid Simulation Approach for Cavity Flows: Blending, Algorithm, and Boundary Treatment Issues," AIAA Journal, Vol. 41, No. 8, pp. 1463-1480, 2003.
  3. Baurle, R.A. and Eklund, D.R. "Analysis of Dual-Mode Hydrocarbon Scramjet Operation at Mach 4--6.5," Journal of Propulsion & Power, Vol. 18, No. 5, pp. 990-1002, 2002.
  4. Baurle, R.A., "Application of Hybrid RANS/LES Methods for the Simulation of Cavity Flowfields," 39th JANNAF Combustion Meeting, Destin, Fl, April 2002.
  5. Smart, M.K. and White, J.A., "Computational Investigation of the Performance and Back-Pressure Limits of a Hypersonic Inlet," AIAA Paper No. 2002-0508, January 2002.
  6. Cockrell, C.E. Jr., Auslender, A.H., White, J.A., and Dilley, A.D., "Aeroheating Predictions for the X-43 Cowl-Closed Configuration at Mach 7 and 10," AIAA Paper No. 2002-0218, January 2002.
  7. Kumar, A., Drummond, J.P., McClinton, C.R., and Hunt, J.L., "Research in Hypersonic Airbreathing Propulsion at the NASA Langley Research Center," Fifteenth International Symposium on Airbreathing Engines, Banalore, India, ISABE-2001: Invited Lecture 4, September 2001.
  8. Baurle, R.A. and Eklund, D.R., "Analysis of a Dual-Mode Hydrocarbon Scramjet at Mach 4-6.5," AIAA Paper No. 2001-3299, July 2001.
  9. Baurle, R.A., Tam, C.-J., Edwards, J.R., and Hassan, H.A., "An Assessment of Boundary Treatment Issues on Hybrid RANS/LES Solution Strategies," AIAA Paper No. 2001-2562, June 2001,
  10. Shebalin, J.-P. and Tiwari, S.N., "NOZ-OP-2D: A CFD-Based Optimization System For Axially Symmetric Rocket Nozzles," AIAA Paper No. 2001-1062, January 2001.
  11. Munipalli, R., Shankar, V., Wilson, D.R., Kim, H.-Y., Lu, F.K., and Liston, G., "Performance Assessment of Ejector Augmented PDR's," AIAA Paper No. 2001-0830, January 2001.
  12. Tam, C.-J. and Baurle, R.A., "Inviscid CFD Analysis of Streamline Traced Hypersonic Inlets at Off-Design Performance," AIAA Paper No. 2001-0675, January 2001.
  13. Smart, M.K., Trexler, C.A., and Goldman, A.L., "A Combined Experimental/Computational Investigation of a Rocket Based Combined Cycle Inlet," AIAA Paper No. 2001-0671, January 2001.
  14. Eklund, D.R., Baurle, R.A., and Gruber, M.R., "Computational Study of a Supersonic Combustor Fueled by an Aerodynamic Ramp Injector," AIAA Paper No. 2001-0379, January 2001.
  15. Cutler, A.D., and White, J.A., "An Experimental and CFD Study of a Supersonic Coaxial Jet," AIAA Paper No. 2001-0143, January 2001.
  16. Rodriguez, C.G., "Asymmetry Effects in the Numerical Simulation of Flows With Upstream Seperated Regions," AIAA Paper No. 2001-0084, January 2001.
  17. Eklund, D.R., Baurle, R.A. and Jackson, T.A., "Investigation of Wall Temperature Effects in a Supersonic Combustor," 37th JANNAF Combustion Meeting, Monterey, CA, November 2000.
  18. Rodriguez, C.G., White, J.A. and Riggins, D.W., "Three-Dimensional Effects in Modeling of Dual Mode Scramjets," AIAA Paper No. 2000-3704, July 2000.
  19. Bobskill, M.V., "Analysis of the AR175 HYPULSE Facility Nozzle," Hyper X Report HX-825, November July 2000.
  20. Rodriguez, C.G., "Simulation of an Experimental Dual-Mode Scramjet(II): Jet-to-Jet Symmetry," Hyper X Report HX-791, March 2000.
  21. Rodriguez, C.G., Riggins, D.W. and Bittner, R.D., "Numerical Simulation of Dual-Mode Scramjet Combustors," 36th JANNAF Combustion Meeting, Monterey, CA, October 1999.
  22. Rodriguez, C.G., "Simulation of an Experimental Dual-Mode Scramjet(I): Mach 2.5 Facility Nozzle," Hyper X Report HX-764, November 99.
  23. Baurle, R.A., Tam C.-J., and Dasgupta, S., "Analysis of Unsteady Cavity Flows for Scramjet Applications," AIAA Paper No. 2000-03617, July 2000.
  24. Rodriguez, C.G., "Simulation of an Experimental Dual-Mode Scramjet: Mach 2.5 Facility Nozzle," Hyper X Report HX-764, November 1999.
  25. Rodriguez, C.G., "Two-Dimensional, Compressible-Flow Test-Cases for Validation of the VULCAN Flow-Solver," Hyper X Report HX-763, November 99.
  26. Shebalin, J.P. and Tiwari S.N., "CFD-Based Optimization of Low Reynolds Number Rocket Nozzles," AIAA Paper No. 99-3794, June 1999.
  27. White, J.A., and Morrison, J.H., "A Pseudo-Temporal Multi-Grid Relaxation Scheme for Solving the Parabolized Navier-Stokes Equations," AIAA Paper No. 99-3360, June 1999.
  28. Tam, C.-J., Baurle, R.A., and Gruber, M.R., "Numerical Study of Jet Injection into a Supersonic Crossflow," AIAA Paper No. 99-2254, 35th June1999.
  29. Eklund, D.R. and Gruber, M.R., "Study of Supersonic Combustor Employing an Aerodynamic Ramp Pilot Injector," AIAA Paper No. 99-2249, June 1999.
  30. Gruber, M.R., Baurle, R.A., Mathur, T., and Hsu, K.-Y.,"Fundamental Studies of Cavity-Based Flame Holder Concepts for Supersonic Combustors," AIAA Paper No. 99-2248, June 1999.
  31. Cox-Stouffer, S.K. and Gruber, M.R., "Further Investigation of the Effects of Aerodynamic Ramp Design Upon Mixing Characteristics," AIAA Paper No. 99-2238, June 1999.
  32. Springer, R.R, Cutler, A.D., Diskin, G.S., and Smith, M.W., "Conventional/Laser Diagnosticsto Assess Flow Quality in a Combustion-Heated Facility," AIAA Paper No. 99-2170, June 1999.
  33. Billig, F.S., Baurle, R.A., Tam, C.-J., and Wornom, S.F., "Design and Analysis of Streamline Traced Hypersonic Inlets," AIAA Paper No. 99-4974, January 1999.
  34. Cox-Stouffer, S.K. and Gruber, M.R., "Effects of Injector Yaw on Mixing Characteristics of Aerodynamic Ramp Injectors," AIAA Paper No. 99-0086, January 1999.
  35. Gaffney, R.L. Jr. and Sanetrik, M.D., "CFD Calculations of the CIAM Scramjet Engine Flowfield," NASA Contractor Report in preparation, 1999.
  36. Baurle, R.A., Cox-Stouffer, S.K., Eklund, D.R., and Gruber, M.R., "An Evaluation of the Nearfield Mixing Effectiveness of Proposed HyTech Combustors," 35th JANNAF Combustion Meeting, Tucson, Az, Dec. 1998.
  37. Cox-Stouffer, S.K. and Gruber, M.R., "Effects of Spanwise Injector Spacing Characteristics of Aerodynamic Ramp Injectors," AIAA Paper No. 98-3272, June 1998.
  38. Baurle, R.A., Mathur, T., Gruber, M.R., and Jackson, K.R., "A Numerical and Experimental Investigation of a Scramjet Combustor for Hypersonic Missile Applications," AIAA Paper No. 98-3121, June 1998.
  39. Baurle, R.A. and Gruber, M.R., "A Study of Recessed Cavity Flowfields for Supersonic Combustion Applications," AIAA Paper No. 98-0938, January 1998.
  40. Baurle, R.A., Fuller, R.P., White, J.A., Chen, T.H., Gruber, M.R., and Nejad, A.S., "An Investigation of Advanced Fuel Injection Scheme for Scramjet Combustion," AIAA Paper No. 98-0937, January 1998.
  41. Alcenius, J.T., Schnieder, S.P., Beckwith, I.E., White, J.A., and Korte, J.J., "Development of Square Nozzles for Supersonic Low-Disturbance Wind Tunnels," Journal of Aircraft, Vol. 33, No. 6, pp. 1131-1138, 1996.
  42. Gaffney, R.L., Jr., White, J.A., Girimaji, S.S., and Drummond, J.P., "Modeling Species Fluctuations in a Turbulent Reacting Flow," Computing Systems in Engineering, Vol. 5, No. 2, pp. 117-133, 1994.
  43. Wilkinson, S.P., Anders, S.G. and White, J.A., "Status of NASA Langley Quiet Tunnel Flow Facility Development," AIAA Paper No. 94-2498, June 1994.
  44. Gaffney, R.L., Jr., White, J.A., Girimaji, S.S., and Drummond, J.P., "Modeling Turbulence / Chemistry Interactions Using Assumed PDF Methods," AIAA Paper No. 92-3638, June 1992.

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This site's most recent update took place: 11/15/2010

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