Linear Stability and Pressure-Driven Response Function of Solid Propellants with Phase Transition
Author:
Affiliation:
1. Politecnico di Milano, 20133 Milan, Italy
2. Russian Academy of Sciences, 117977, Moscow, Russia
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/10.2514/2.5500
Reference42 articles.
1. Surface Temperature Measurements on Burning Solids1a
2. Meyer. R., Explosives, 2nd ed.Verlag Chemie, Weinheim, Germany, 1981, pp.16-18.
3. A model of ammonium perchlorate deflagration between 20 and 100 atm
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