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Thomas L Jackson
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Year
7.1 Combustion and Energetic Materials
J Buckmaster, TL Jackson, L Massa, M Ulrich
7.1 Program Overview
J Buckmaster, M Chen, TL Jackson, L Massa
2002
A high-order incompressible flow solver with WENO
J Zhang, TL Jackson
Journal of Computational Physics 228 (7), 2426-2442, 2009
552009
A model for erosive burning of homogeneous propellants
J Zhang, TL Jackson
Combustion and Flame 157 (2), 397-407, 2010
302010
A new packing code for creating mirostructures of propellants and explosives
G Amadio, TL Jackson
51st AIAA/SAE/ASEE Joint Propulsion Conference, 4098, 2015
152015
A new proxy application for compressible multiphase turbulent flows
T Banerjee, J Hackl, M Shringarpure, T Islam, S Balachandar, T Jackson, ...
Sustainable Computing: Informatics and Systems 16, 11-24, 2017
32017
A numerical study of periodic sandwich propellants with oxygenated binders
X Zhou, TL Jackson, J Buckmaster
Combustion Theory and Modelling 7 (2), 435, 2003
132003
A simplified model for composite propellant burning rate
G Knott, M Brewster, T Jackson
37th Aerospace Sciences Meeting and Exhibit, 591, 1999
41999
Absolute–convective instabilities and their associated wave packets in a compressible reacting mixing layer
FQ Hu, TL Jackson, DG Lasseigne, CE Grosch
Physics of Fluids A: Fluid Dynamics 5 (4), 901-915, 1993
111993
Absolute/convective instabilities and the convective Mach number in a compressible mixing layer
TL Jackson, CE Grosch
101989
Absolute/convective instabilities and the convective Mach number in a compressible mixing layer
TL Jackson, CE Grosch
Physics of Fluids A: Fluid Dynamics 2 (6), 949-954, 1990
761990
Absolute/convective instabilities and the convective Mach number in a compressible mixing layer(Final Report)
TL JACKSON, CE GROSCH
1989
Acoustics in a two-dimensional slab rocket motor
Y Daimon, T Jackson, V Topalian, J Freund, J Buckmaster
46th AIAA Aerospace Sciences Meeting and Exhibit, 1006, 2008
12008
Agglomeration in solid rocket propellants: novel experimental and modeling methods
F Maggi, A Bandera, LT De Luca, V Thoorens, JF Trubert, TL Jackson
Progress in propulsion Physics 2, 81-98, 2011
382011
Aluminum agglomeration modeling using a packing code
F Maggi, T Jackson, J Buckmaster
46th AIAA Aerospace Sciences Meeting and Exhibit, 940, 2008
52008
An aluminum injection model based on random packs for solid propellant rocket motor simulations
T Jackson, F Najjar, J Buckmaster
40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 4042, 2004
32004
An asymptotic analysis of supersonic reacting mixing layers
TL Jackson, MY Hussaini
41987
An asymptotic analysis of supersonic reacting mixing layers
TL Jackson, MY Hussaini
Combustion science and technology 57 (4-6), 129-140, 1988
631988
An elementary discussion of propellant flame geometry
J Buckmaster, TL Jackson, J Yao
Combustion and Flame 117 (3), 541-552, 1999
581999
An examination of the shrinking-core model of sub-micron aluminum combustion
J Buckmaster, TL Jackson
Combustion Theory and Modelling 17 (2), 335-353, 2013
172013
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