Liquid Films Instability Analysis of Liquefying Hybrid Rocket Fuels Under Supercritical Conditions
Author:
Affiliation:
1. Department of Aeronautics and Astronautics, University of Tokyo, Tokyo 113-0033, Japan
2. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Kanagawa 252-0222, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053459
Reference10 articles.
1. Combustion of Liquefying Hybrid Propellants: Part 1, General Theory
2. Evaluation of the Homologous Series of Normal Alkanes as Hybrid Rocket Fuels
3. On the Thermodynamics of Solutions. V. An Equation of State. Fugacities of Gaseous Solutions.
4. A New Two-Constant Equation of State
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