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International Journal of Energetic Materials and Chemical Propulsion
ESCI SJR: 0.28 SNIP: 0.421 CiteScore™: 0.9

ISSN Imprimer: 2150-766X
ISSN En ligne: 2150-7678

International Journal of Energetic Materials and Chemical Propulsion

DOI: 10.1615/IntJEnergeticMaterialsChemProp.v7.i5.50
pages 421-436

NUMERICAL SIMULATION OF JP-10/AIR TWO-PHASE DETONATION

Naomichi Masuda
Department of Mechanical Engineering, Aoyama Gakuin University, Kanagawa, Japan
Venkat Tangirala
Combustion and Propulsion, Energy and Propulsion Technology, Global Research Center, General Electric Company, USA
Krzytof Benkiewicz
Warsaw Institute of Aviation and General Electric (GE) Aviation, Warsaw,Poland
A. Koichi Hayashi
Department of Mechanical Engineering, Aoyama Gakuin University, Kanagawa, Japan
Nobuyuki Tsuboi
Kyushu Institute of Technology

RÉSUMÉ

JP-10/air two-phase detonation is numerically studied using the Eulerian code to determine the accuracy of the numerical approach by comparing detonation velocities among three groups: the present study, Tangirala and Dean, and Cheatham and Kailasanath. It was found within those studies that JP-10/air detonation velocities were identical, leading to the conclusion that the present method was valid and numerical simulation could proceed. A two-dimensional numerical study was performed using a commercial code and it was discovered that the detonation velocity of a JP-10 droplet/air mixture (3 micron droplet case) is within 5% lower than that of a JP-10 gas/air mixture and that the Ispf of Pulse Detonation Engine (PDE) initially fueled with a gas/air mixture is slightly higher than that of a PDE initially fueled with a multiphase JP10 liquid/air mixture.

RÉFÉRENCES

  1. Cheatham, S. and Kailasanath, K., Numerical Simulations of Multiphase Detonations in Tubes.

  2. Cheatham, S. and Kailasanath, K., Multiphase Detonations in Pulse Detonation Engines.

  3. Cheatham, S. and Kailasanath, K., Single-Cycle Performance of Idealized Liquid-Fueled Pulse Detonation Engines.

  4. Varatharajan, B., Petrova, M., Williams, F.A., and Tangirala, V., Two-Step Chemical-Kinetic Descriptions for Hydrocarbon-Oxygen-Diluent Ignition and Detonation Applications.

  5. Schauer, F.R., Miser, C.L., and Tucker, K.C., Detonation Initiation of Hydrocarbon-Air Mixtures in a Pulsed Detonation Engine.

  6. Tangirala, V. and Dean, A.J., Investigations of Two-Phase Detonations for Performance Estimations of a Pulse Detonation Engine.

  7. Reynolds, W.C., STANJAN Chemical Equilibrium Solver.

  8. Kee, J., Warnatz, J., and Miller, J.A., A FORTRAN Computer Code Package for Evaluation of Gas-Phase Viscosities, Conductivities, and Diffusion Coefficients.

  9. Benkiewicz, K. and Hayashi, A.K., Aluminum Dust Ignition behind Reflected Shock Wave, Two-Dimensional Simulations.

  10. Brophy, C.M., Netzer, D.W., Sinibaldi, J., and Johnson, J., Detonation of a JP-10 Aerosol for Pulse Detonation Applications.

  11. Chakravarthy, S., Goldberg, U., Batten, P., Palaniswamy, S., and Peroomian, O., Some Recent Progress in Practical Computational Fluid Dynamics.

  12. Tangirala, V.E., Varatharajan, B., and Dean, A.J., Numerical Simulations of Direct Initiation of Detonations in Hydrocarbon Fuel/Air Mixtures.

  13. Tangirala, V.E., Dean, A.J., Rasheed, A., and Chapin, D.M., Performance Estimates of a Pulsed Detonation Engine.

  14. Tangirala, V.E., Dean, A.J., Pinard, P.F., and Chapin, D.M., Investigation of Cyclic Pulsed Detonation Processes, Experiments and Calculations.

  15. Tangirala, V.E., Dean, A.J., Pinard, P.F., and Varatharajan, B., Investigation of Cycle Processes in a Pulsed Detonation Engine Operating on Fuel-Air Mixtures.

  16. Cheatham, S. and Kailasanath, K., Numerical Modeling of Liquid-Fueled Detonation in Tubes.

  17. Wintenberger, E., Austin, J.M., Cooper, M., Jackson, S., and Shepherd, J.E., An Analytical Model for the Impulse of a Single-Cycle Pulse Detonation Engine.


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