Progress in Propulsion Physics – Volume 2
Versailles, France, July 6-10, 2009L.T. DeLuca, C. Bonnal, O. Haidn and S.M. Frolov (Eds.)
ISBN: 978-2-7598-0673-7
Solid Rocket Propulsion
Open Access
Issues related to heterogeneous solid-propellant combustion p. 3
Published online: 01 October 2012
Open Access
Heterogeneous solid propellants: from microstructure to macroscale properties p. 21
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Open Access
Heterogeneous propellant internal ballistics: criticism and regeneration p. 35
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Open Access
The cohesive law of particle/binder interfaces in solid propellants p. 59
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Open Access
Ballistic effectiveness of superdense solid composite propellants with zirconium or zirconium hydride p. 67
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Open Access
Agglomeration in solid rocket propellants: novel experimental and modeling methods p. 81
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Open Access
Characterization of nal powders for rocket propulsion p. 99
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Open Access
Light deviation based optical techniques applied to solid propellant combustion p. 121
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Open Access
Ultrasonic measurements of burning rates in full-size rocket motors p. 135
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Open Access
Ariane 5 solid rocket booster dynamic behavior with respect to pressure oscillations p. 149
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Liquid Rocket Propulsion
Open Access
Fluid disintegration studies in a specialized shock tube p. 165
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Open Access
Lagrangian modeling of turbulent spray combustion: application to rocket engines cryogenic conditions p. 207
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Open Access
Numerical investigation of destabilization of supercritical round turbulent jets using large eddy simulation p. 225
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Open Access
Improved heat transfer prediction engineering capabilities for rocket thrust chamber layout p. 239
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Open Access
Combustion efficiency of a porous injector during throttling of a LOx/H2 combustion chamber p. 251
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Open Access
Advanced altitude simulation facility P8 − current status p. 265
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Open Access
Consideration of real gas effects and condensation in a spray-combustion rocket-thrust-chamber design tool p. 285
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Open Access
Integrated method for combustion stability prediction p. 297
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Open Access
High-frequency instabilities in rocket thrust chambers: an engineering approach p. 317
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Open Access
On the acoustics of rocket combustors equipped with quarter wave absorbers p. 339
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Hybrid Rocket Propulsion
Open Access
Various challenging aspects of hybrid propulsion p. 375
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Open Access
The characteristics of turbulent surface flow in planar channel with imposed wall blowing p. 389
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Open Access
Time-resolved burning of solid fuels for hybrid rocket propulsion p. 405
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Air-Breathing Propulsion
Open Access
Investigation of performances of innovative aeronautic injection systems using advanced laser diagnostics p. 429
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Open Access
Effect of nonconformances on the aerodynamic performance of low-pressure turbine outlet guide vanes p. 445
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Open Access
Effects of particle mixing and scattering in the dusty gas flow through moving and stationary cascades of airfoils p. 459
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Open Access
Modification and testing of an engine and fuel control system for a hydrogen fuelled gas turbine p. 475
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Open Access
The performance of a boron-loaded gel-fuel ramjet p. 499
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Open Access
Electrically driven combustion near the plane wall in a supersonic duct p. 519
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Detonation Engines
Open Access
Numerical simulation of deflagration-to-detonation transition by coupled flame tracking - particle method p. 533
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Open Access
Experimental and numerical study of the rotating detonation engine in hydrogen-air mixtures p. 555
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Electric Thrusters
Open Access
Experimental and numerical studies of a direct current microdischarge plasma thruster p. 585
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Open Access
Elementary scaling laws for the design of low and high power hall effect thrusters p. 601
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Open Access
Investigation of discharge channel wall material influence on lifetime of hall effect thruster with high specific impulse p. 617
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Open Access
Electric propulsion systems for small satellites: the low earth orbit mission perseus p. 629
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Thrust Nozzles
Open Access
Experimental study of a planar expansion-deflection nozzle p. 641
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Open Access
Wall pressure and thrust of a dual bell nozzle in a cold gas facility p. 655
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Open Access
Optimization of supersonic axisymmetric nozzles with a center body for aerospace propulsion p. 675
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Propulsion System and Subsystem Design
Open Access
Carmen, liquid propulsion systems simulation platform p. 695
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Open Access
A fast engineering tool for simulation and design of propellant management systems in liquid propelled launcher stages p. 707
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Open Access
Numerical analysis of propellant behavior in tanks: from small-scale to industrial models p. 717
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Open Access
Fluid-structure interaction modeling: first applications at cnes p. 727
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Open Access
Satellite propulsion modeling with ecosimpro: comparison between simulation and ground tests p. 743
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Open Access
Aerothermal and flight mechanic considerations by development of small launchers for low orbit payloads started from lorentz rail accelerator p. 765
Published online: 01 October 2012