Crossref Citations
This article has been cited by the following publications. This list is generated based on data provided by
Crossref.
Daimon, Y.
Jackson, T. L.
Topalian, V.
Freund, J. B.
and
Buckmaster, J.
2009.
Effect of propellant morphology on acoustics in a planar rocket motor.
Theoretical and Computational Fluid Dynamics,
Vol. 23,
Issue. 1,
p.
63.
Isfahani, Amir
Zhang, Ju
and
Jackson, Thomas
2009.
Erosive Burning of Homogeneous and Heterogeneous Solid Propellants.
Zhang, Ju
Jackson, Thomas
Najjar, Fady
and
Buckmaster, John
2009.
High-Fidelity Multiphase Simulations of Erosion in SRM Nozzles.
Jackson, Thomas
Zhang, Ju
and
Topalian, V.
2010.
Erosive Burning of Solid Propellants.
Jackson, Thomas L.
and
Austin, Joanna M.
2010.
Encyclopedia of Aerospace Engineering.
Zhang, Ju
Jackson, Thomas L.
Buckmaster, John
and
Najjar, Fady
2011.
Erosion in Solid-Propellant Rocket Motor Nozzles with Unsteady Nonuniform Inlet Conditions.
Journal of Propulsion and Power,
Vol. 27,
Issue. 3,
p.
642.
Hedman, Trevor
Cho, Kevin
Satija, Aman
Groven, Lori
Lucht, Robert
and
Son, Steven
2011.
Flame Structure of a Bimodal Ammonium Perchlorate Composite Propellant Using 5kHz PLIF.
Jackson, Thomas L.
2012.
Modeling of Heterogeneous Propellant Combustion: A Survey.
AIAA Journal,
Vol. 50,
Issue. 5,
p.
993.
Hedman, T.D.
Cho, K.Y.
Satija, A.
Groven, L.J.
Lucht, R.P.
and
Son, S.F.
2012.
Experimental observation of the flame structure of a bimodal ammonium perchlorate composite propellant using 5 kHz PLIF.
Combustion and Flame,
Vol. 159,
Issue. 1,
p.
427.
Hedman, T.D.
Groven, L.J.
Cho, K.Y.
Lucht, R.P.
and
Son, S.F.
2013.
The diffusion flame structure of an ammonium perchlorate based composite propellant at elevated pressures.
Proceedings of the Combustion Institute,
Vol. 34,
Issue. 1,
p.
649.
Hedman, Trevor D.
Groven, Lori J.
Lucht, Robert P.
and
Son, Steven F.
2013.
The effect of polymeric binder on composite propellant flame structure investigated with 5 kHz OH PLIF.
Combustion and Flame,
Vol. 160,
Issue. 8,
p.
1531.
Dierich, Frank
and
Wittig, Kay
2014.
Gasification Processes.
p.
171.
Gallier, Stany
and
Plaud, Mathieu
2019.
A model for solid propellant burning fluctuations using mesoscale simulations.
Acta Astronautica,
Vol. 158,
Issue. ,
p.
296.
Gallier, Stany
and
Plaud, Mathieu
2019.
Vorticoacoustic Stability of Solid Rocket Motors: A Numerical Study.
Journal of Propulsion and Power,
Vol. 35,
Issue. 4,
p.
787.
Mehrabadi, Mohammad
Safdari, Masoud
Dick, William
and
Jackson, Thomas L.
2021.
Effect of Pressure on the Fluctuations above a Burning Heterogeneous Propellant.
Zhang, Yanrong
Cang, Yu
Yang, Shuo
and
Wang, Lipo
2022.
Heterogeneous propellant combustion with conjugated interface conditions.
Computers & Fluids,
Vol. 240,
Issue. ,
p.
105397.
Cang, Yu
Hu, Yue
Wang, Lipo
and
Shen, Yongxing
2022.
Numerical scheme solving the temperature of the interface between gas and heterogeneous solid with phase change.
International Journal for Numerical Methods in Engineering,
Vol. 123,
Issue. 4,
p.
1036.
Chen, Kaixuan
Ye, Zhenwei
Yu, Yizhe
Xue, Xiaochun
and
Yu, Yonggang
2023.
Unsteady heat and mass transfer mechanism in AP/HTPB propellant combustion under rapid depressurization.
International Communications in Heat and Mass Transfer,
Vol. 146,
Issue. ,
p.
106949.
Di Mascio, Andrea
Martelli, Emanuele
Bernardini, Matteo
Stella, Fulvio
and
Neri, Agostino
2023.
Boundary Conditions for Inhomogeneous Combustion Simulation in Solid Rocket Motors.
AIAA Journal,
Vol. 61,
Issue. 5,
p.
2314.
Chen, Kaixuan
Xue, Xiaochun
and
Yu, Yonggang
2024.
Modeling transient combustion and regression behavior of NEPE propellant based on random particle packing.
Applied Mathematical Modelling,
Vol. 126,
Issue. ,
p.
85.