Year |
Citation |
Score |
2016 |
Stechmann D, Heister SD, Sardeshmukh S. High-pressure rotating detonation engine testing and flameholding analysis with hydrogen and natural gas 52nd Aiaa/Sae/Asee Joint Propulsion Conference, 2016. |
0.66 |
|
2016 |
Anderson WS, Lim D, Washington MR, Heister SD. Experimental study of liquid injector elements for use in rotating detonation engines 52nd Aiaa/Sae/Asee Joint Propulsion Conference, 2016. |
0.333 |
|
2016 |
Mikoshiba K, Sardeshmukh SV, Stechmann D, Heister SD. Numerical studies of dynamic response for an oxidizer injector to detonation wave 52nd Aiaa/Sae/Asee Joint Propulsion Conference, 2016. |
0.646 |
|
2014 |
Sardeshmukh SV, Heister SD. Reacting opposed jets of hypergolic propellants MMH and RFNA 50th Aiaa/Asme/Sae/Asee Joint Propulsion Conference 2014. DOI: 10.2514/6.2014-3565 |
0.647 |
|
2014 |
Heister SD, Steen DA, Sardeshmukh SV. Computational simulation of a counter-rotating vortex pair mixer for aerospace applications 50th Aiaa/Asme/Sae/Asee Joint Propulsion Conference 2014. DOI: 10.2514/6.2014-3543 |
0.619 |
|
2013 |
Sardeshmukh SV, Heister SD, Wang H, Sankaran V. Kinetics modeling of hypergolic propellants 49th Aiaa/Asme/Sae/Asee Joint Propulsion Conference. |
0.591 |
|
2013 |
Sun Park K, Sardeshmukh SV, Heister SD, Sankaran V. Numerical simulation of combustion of unlike impinging jets near a wall 49th Aiaa/Asme/Sae/Asee Joint Propulsion Conference. |
0.648 |
|
2012 |
Sardeshmukh SV, Heister SD, Xia G, Merkle C. Kinetic modeling of hypergolic propellants using impinging element injectors 48th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2012. |
0.675 |
|
2011 |
Bang BH, Yoon SS, Kim HY, Heister SD, Park H, James SC. Assessment of gas and liquid velocities induced by an impacting liquid drop International Journal of Multiphase Flow. 37: 55-66. DOI: 10.1016/J.Ijmultiphaseflow.2010.08.008 |
0.353 |
|
2008 |
Park H, Yoon SS, Jepsen RA, Heister SD, Kim HY. Droplet bounce simulations and air pressure effects on the deformation of pre-impact droplets, using a boundary element method Engineering Analysis With Boundary Elements. 32: 21-31. DOI: 10.1016/J.Enganabound.2007.07.002 |
0.368 |
|
2005 |
Kim BD, Heister SD, Collicott SH. Three-dimensional flow simulations in the recessed region of a coaxial injector Journal of Propulsion and Power. 21: 728-742. DOI: 10.2514/1.12651 |
0.337 |
|
2002 |
Weinstock VD, Heister SD. Modeling oil flows in engine sumps: Drop dynamics and wall impact simulation 38th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. DOI: 10.1115/1.1924432 |
0.303 |
|
2001 |
Xu C, Blaisdell GA, Heister SD. Simulations of turbulent, cavitating flows in an injector slot/orifice Advances in Fluid Mechanics. 29: 185-195. |
0.3 |
|
2000 |
Bunnell RA, Heister SD. Three-dimensional unsteady simulation of cavitating flows in injector passages Journal of Fluids Engineering, Transactions of the Asme. 122: 791-797. DOI: 10.1115/1.1315590 |
0.304 |
|
1998 |
Rump KM, Heister SD. Modeling the effect of unsteady chamber conditions on atomization processes Journal of Propulsion and Power. 14: 576-579. DOI: 10.2514/2.7645 |
0.348 |
|
1997 |
Rump KM, Heister SD. Modeling the effect of unsteady chamber condtions on atomization processes 33rd Joint Propulsion Conference and Exhibit. |
0.36 |
|
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