Year |
Citation |
Score |
2019 |
Stechmann DP, Sardeshmukh S, Heister SD, Mikoshiba K. Role of Ignition Delay in Rotating Detonation Engine Performance and Operability Journal of Propulsion and Power. 35: 125-140. DOI: 10.2514/1.B37117 |
0.508 |
|
2018 |
Schwinn K, Gejji R, Kan B, Sardeshmukh S, Heister S, Slabaugh CD. Self-sustained, high-frequency detonation wave generation in a semi-bounded channel Combustion and Flame. 193: 384-396. DOI: 10.1016/J.Combustflame.2018.03.022 |
0.536 |
|
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. |
0.558 |
|
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. |
0.527 |
|
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 |
0.589 |
|
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 |
0.567 |
|
2014 |
Bedard MJ, Sardeshmukh SV, Fuller TL, Anderson WE, Tanabe M. Chemiluminescence as a diagnostic in studying combustion instability in a practical combustor 50th Aiaa/Asme/Sae/Asee Joint Propulsion Conference 2014. DOI: 10.1016/J.Combustflame.2019.11.039 |
0.38 |
|
2013 |
Sardeshmukh SV, Heister SD, Wang H, Sankaran V. Kinetics modeling of hypergolic propellants 49th Aiaa/Asme/Sae/Asee Joint Propulsion Conference. |
0.535 |
|
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. |
0.599 |
|
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. |
0.621 |
|
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