Numerical Study of Cryogenic Jets Under Supercritical Conditions
Author:
Affiliation:
1. Universidade da Beira Interior, 6201-001 Covilha, Portugal
2. Centre National de la Recherche Scientique, 45071 Orleans Cedex 2, 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/10.2514/2.6090
Reference20 articles.
1. Propellant injection in a liquid oxygen/gaseous hydrogen rocket engine
2. Atomization and Breakup of Cryogenic Propellants Under High-Pressure Subcritical and Supercritical Conditions
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