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Numerical analysis of a ram accelerator employing two-phase combustion

Published:1996-07 Issue:4 Volume:12 Page:708-717
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Saurel Richard¹

Affiliation:

1. Universite de Provence, 13397 Marseille, France

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.24092

Reference34 articles.

1. Ram accelerator - A new chemical method for accelerating projectilesto ultrahigh velocities

2. Experimental investigation of ram accelerator propulsion modes

3. Ram accelerator direct space launch system - New concepts

4. Computational investigation of oblique detonation ramjet-in-tube concepts

5. Calculations for steady propagation of a generic ram accelerator configuration

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1. Experimental Investigation and Numerical Simulation of Secondary Combustor Flow in Boron-Based Propellant Ducted Rocket;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2013

2. Review of Multiscale Modeling of Detonation;Journal of Propulsion and Power;2006-11

3. Numerical simulation of detonations in mixtures of gases and solid particles;Journal of Fluid Mechanics;2004-05-25

4. Kinetic Model for Aluminum-Sensitized Ram Accelerator Combustion;Journal of Propulsion and Power;2003-03

5. A multiphase model for compressible flows with interfaces, shocks, detonation waves and cavitation;Journal of Fluid Mechanics;2001-03-25

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