This report results from a contract tasking Dipanmento Di Ingegneria Aerospaziale as follows: The contractor will review Russian works on response function of solid propellant combustion to oscillatory pressure and on acoustic admittance. Differences and similarities between US and Russian approaches to this problem shall be considered.
Nonlinear Interaction Between Acoustics and Propellant Combustion
1996
42 pages
Report
Keine Angabe
Englisch
Combustion & Ignition , Rocket Propellants , Burning rate , Solid rocket propellants , Pressure gradients , Mathematical models , Thermal diffusion , Partial differential equations , Russia , Unsteady flow , Flame propagation , Combustion stability , Integral equations , Acoustic properties , Propellant burn out , United kingdom , Foreign technology , Foreign reports
Nonlinear Heterogeneous Model of Composite Solid-Propellant Combustion
Online Contents | 2002
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