Chemically Driven

  1. Vyas, A. B. and Majdalani, J., Asymptotic Temperature Distribution in a Simulated Combustion Chamber, Journal of Heat Transfer, Vol. 129, No. 7, July 2007, pp. 894-898.

  2. Vyas, A. B., Majdalani, J. and Yang, V., Estimation of the Laminar Premixed Flame Temperature and Velocity in Injection-Driven Combustion Chambers, Combustion and Flame, Vol. 133, No. 6129, May 2003, pp. 371–374.

  3. Chu, W.-W., Yang, V. and Majdalani, J., Premixed Flame Response to Acoustic Waves in a Porous-Walled Chamber with Surface Mass Injection, Combustion and Flame, Vol. 133, No. 6129, May 2003, pp. 359–370.

  4. Majdalani, J., Physicality of Core Flow Models in Rocket Motors, Journal of Propulsion and Power, Vol. 19, No. 1, January 2003, pp. 156–159.

  5. Entezam, B., Van Moorhem, W. K. and Majdalani, J., Two-Dimensional Numerical Verification of the Unsteady Thermoacoustic Field Inside a Rijke-Type Pulse Combustor, Journal of Numerical Heat Transfer: A–Applications, Vol. 41, No. 3, 2002, pp. 245–262.

  6. Chu, W.-W., Yang, V., Vyas, A. B. and Majdalani, J., Diffusion Flame Structure in a Simulated Slab Rocket Motor, International Workshop on High-Energy Materials: Demilitarization and Civil Applications, Biysk Belokurikha, Russia, September 2004.

  7. Fang. D., Majdalani, J. and Chiaverini, M. J., Hot Flow Model of the Vortex Cold Wall Liquid Rocket, AIAA-2004-3676, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Ft Lauderdale, FL, July 11-14, 2004.

  8. Fang, D. Q., Majdalani, J. and Chiaverini, M. J., Simulation of the Cold-Wall Swirl Driven Combustion Chamber, AIAA-2003-5055, 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, AL, July 20-23, 2003.

  9. Chiaverini, M. J., Malecki, M. J., Sauer, A., Knuth, W. H., Gramer, D. J. and Majdalani, J., Vortex Thrust Chamber Testing and Analysis for O2-H2 Propulsion Applications, AIAA-2003-4473, 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, AL, July 20-23, 2003.

  10. Chu, W.-W., Yang, V., Vyas, A. B., and Majdalani, Premixed Flame Response to Acoustic Waves in a Porous-Walled Chamber with Surface Mass Injection, AIAA-2002-3609, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Indianapolis, IN, July 7-10, 2002.

  11. Majdalani, J., Entezam, B. and Van Moorhem, W. K., The Rijke Tube Revisited via Laboratory and Numerical Experiments, AIAA-2001-2961, 35th AIAA Thermophysics Conference, Anaheim, CA, June 11-14, 2001.

  12. Majdalani, J., Entezam, B. and Van Moorhem, W. K., Full-Scale Numerical Model of a Rijke-Type Pulse Combustor, AIAA-2001-2121, 7th AIAA/CEAS Aeroacoustics Conference, Maastricht, The Netherlands, May 28-30, 2001.

  13. Entezam, B., Van Moorhem, W. K. and Majdalani, J., A Novel Investigation of the Thermoacoustic Fields Inside a Rijke Tube, AIAA-98-2582, 7th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, Albuquerque, NM, June 15-18, 1998.

  14. Entezam, B., Van Moorhem, W. K. and Majdalani, J., Modeling of a Rijke-Tube Pulse Combustor Using Computational Fluid Dynamics, AIAA-97-2718, 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Seattle, WA, July 6-9, 1997.