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Progress in Propulsion Physics
Latest Publications
TOTAL DOCUMENTS
46
(FIVE YEARS 0)
H-INDEX
6
(FIVE YEARS 0)
Published By EDP Sciences
9782759806737, 9782759806881
Latest Documents
Most Cited Documents
Contributed Authors
Related Sources
Related Keywords
Latest Documents
Most Cited Documents
Contributed Authors
Related Sources
Related Keywords
Lagrangian modeling of turbulent spray combustion: application to rocket engines cryogenic conditions
Progress in Propulsion Physics
◽
10.1051/eucass/201102207
◽
2011
◽
Cited By ~ 5
Author(s):
J.-F. Izard
◽
A. Mura
Keyword(s):
Spray Combustion
◽
Rocket Engines
◽
Lagrangian Modeling
◽
Turbulent Spray Combustion
◽
Turbulent Spray
◽
Cryogenic Conditions
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Numerical simulation of deflagration-to-detonation transition by coupled flame tracking - particle method
Progress in Propulsion Physics
◽
10.1051/eucass/201102533
◽
2011
◽
Author(s):
S. M. Frolov
◽
V. S. Ivanov
Keyword(s):
Numerical Simulation
◽
Particle Method
◽
Deflagration To Detonation Transition
◽
Detonation Transition
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Experimental and numerical study of the rotating detonation engine in hydrogen-air mixtures
Progress in Propulsion Physics
◽
10.1051/eucass/201102555
◽
2011
◽
Cited By ~ 33
Author(s):
J. Kindracki
◽
A. Kobiera
◽
P. Wolański
◽
Z. Gut
◽
M. Folusiak
◽
...
Keyword(s):
Numerical Study
◽
Rotating Detonation Engine
◽
Detonation Engine
◽
Rotating Detonation
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On the acoustics of rocket combustors equipped with quarter wave absorbers
Progress in Propulsion Physics
◽
10.1051/eucass/201102339
◽
2011
◽
Cited By ~ 1
Author(s):
M. Oschwald
◽
M. Marpert
Keyword(s):
Quarter Wave
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Advanced altitude simulation facility P8 − current status
Progress in Propulsion Physics
◽
10.1051/eucass/201102265
◽
2011
◽
Author(s):
C. Pauly
◽
D. Suslov
◽
O. J. Haidn
Keyword(s):
Current Status
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Improved heat transfer prediction engineering capabilities for rocket thrust chamber layout
Progress in Propulsion Physics
◽
10.1051/eucass/201102239
◽
2011
◽
Cited By ~ 2
Author(s):
C. Maeding
◽
D. Wiedmann
◽
K. Quering
◽
O. Knab
Keyword(s):
Heat Transfer
◽
Thrust Chamber
◽
Rocket Thrust
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Ballistic effectiveness of superdense solid composite propellants with zirconium or zirconium hydride
Progress in Propulsion Physics
◽
10.1051/eucass/201102067
◽
2011
◽
Author(s):
D. Lempert
◽
G. Manelis
◽
G. Nechiporenko
Keyword(s):
Zirconium Hydride
◽
Solid Composite Propellants
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Various challenging aspects of hybrid propulsion
Progress in Propulsion Physics
◽
10.1051/eucass/201102375
◽
2011
◽
Author(s):
O. Orlandi
◽
D. Theil
◽
J. Saramago
◽
P. G. Amand
◽
F. Dauch
◽
...
Keyword(s):
Hybrid Propulsion
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Time-resolved burning of solid fuels for hybrid rocket propulsion
Progress in Propulsion Physics
◽
10.1051/eucass/201102405
◽
2011
◽
Cited By ~ 18
Author(s):
L.T. DeLuca
◽
L. Galfetti
◽
G. Colombo
◽
F. Maggi
◽
A. Bandera
◽
...
Keyword(s):
Solid Fuels
◽
Hybrid Rocket
◽
Time Resolved
◽
Rocket Propulsion
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The cohesive law of particle/binder interfaces in solid propellants
Progress in Propulsion Physics
◽
10.1051/eucass/201102059
◽
2011
◽
Cited By ~ 1
Author(s):
H. Tan
Keyword(s):
Solid Propellants
◽
Cohesive Law
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