| Year |
Citation |
Score |
| 2020 |
Walters IV, Journell CL, Lemcherfi A, Gejji RM, Heister SD, Slabaugh CD. Operability of a Natural Gas–Air Rotating Detonation Engine Journal of Propulsion and Power. 36: 453-464. DOI: 10.2514/1.B37735 |
0.309 |
|
| 2020 |
Anderson WS, Heister SD, Kan B, Hartsfield C. Experimental Study of a Hypergolically Ignited Liquid Bipropellant Rotating Detonation Rocket Engine Journal of Propulsion and Power. 1-11. DOI: 10.2514/1.B37666 |
0.348 |
|
| 2020 |
Mikoshiba K, Sardeshmukh SV, Heister SD. On the response of annular injectors to rotating detonation waves Shock Waves. 30: 29-40. DOI: 10.1007/S00193-019-00900-8 |
0.382 |
|
| 2019 |
Stechmann DP, Heister SD, Harroun AJ. Rotating Detonation Engine Performance Model for Rocket Applications Journal of Spacecraft and Rockets. 56: 887-898. DOI: 10.2514/1.A34313 |
0.31 |
|
| 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 |
0.347 |
|
| 2017 |
Kan BK, Heister SD, Paxson DE. Experimental Study of Pressure Gain Combustion with Hypergolic Rocket Propellants Journal of Propulsion and Power. 33: 112-120. DOI: 10.2514/1.B36195 |
0.379 |
|
| 2016 |
Shark SC, Zaseck CR, Pourpoint TL, Son SF, Heister SD. Performance and flame visualization of dicyclopentadiene rocket propellants with metal hydride additives Journal of Propulsion and Power. 32: 869-881. DOI: 10.2514/1.B35853 |
0.786 |
|
| 2016 |
Thompson AS, Heister SD. Characteristics of flashing flows within a high aspect ratio injector Atomization and Sprays. 26: 633-658. DOI: 10.1615/Atomizspr.2015011677 |
0.404 |
|
| 2016 |
Thompson AS, Heister SD. Visualization of cavitating flow within a high-aspect-ratio slot injector Atomization and Sprays. 26: 93-119. DOI: 10.1615/Atomizspr.2015011356 |
0.31 |
|
| 2015 |
Kumar S, Heister SD, Xu X, Salvador JR. Optimization of Thermoelectric Components for Automobile Waste Heat Recovery Systems Journal of Electronic Materials. 44: 3627-3636. DOI: 10.1007/S11664-015-3912-4 |
0.547 |
|
| 2014 |
Wiest HK, Heister SD. Experimental study of gas turbine combustion with elevated fuel temperatures Journal of Engineering For Gas Turbines and Power. 136. DOI: 10.1115/1.4027907 |
0.372 |
|
| 2014 |
Yoon C, Heister SD, Campanella OH. Modeling gelled fluid flow with thixotropy and rheological hysteresis effects Fuel. 128: 467-475. DOI: 10.1016/J.Fuel.2014.02.051 |
0.612 |
|
| 2013 |
Shark SC, Pourpoint TL, Son SF, Heister SD. Performance of dicyclopentadiene/H2O2-based hybrid rocket motors with metal hydride additives Journal of Propulsion and Power. 29: 1122-1129. DOI: 10.2514/1.B34867 |
0.78 |
|
| 2013 |
Rettenmaier AK, Heister SD. Experimental study of erosive and dynamic burning in polybutadiene-based composite propellants Journal of Propulsion and Power. 29: 87-94. DOI: 10.2514/1.B34668 |
0.323 |
|
| 2013 |
Dambach EM, Solomon Y, Heister SD, Pourpoint TL. Investigation into the hypergolic ignition process initiated by low weber number collisions Journal of Propulsion and Power. 29: 331-338. DOI: 10.2514/1.B34627 |
0.779 |
|
| 2013 |
Yoon C, Heister SD, Merkle CL, Guoping Xia. Simulations of plain-orifice injection of gelled propellants under manifold crossflow conditions Journal of Propulsion and Power. 29: 136-146. DOI: 10.2514/1.B34610 |
0.624 |
|
| 2013 |
Trebs A, Heister SD. Improved injector metrics for supersonic combustors Journal of Propulsion and Power. 29: 274-275. DOI: 10.2514/1.B34589 |
0.77 |
|
| 2013 |
Park KS, Heister SD. Modeling particle collision processes in high Reynolds number flow Journal of Aerosol Science. 66: 123-138. DOI: 10.1016/J.Jaerosci.2013.08.010 |
0.467 |
|
| 2013 |
Kumar S, Heister SD, Xu X, Salvador JR, Meisner GP. Thermoelectric generators for automotive waste heat recovery systems part II: Parametric evaluation and topological studies Journal of Electronic Materials. 42: 944-955. DOI: 10.1007/S11664-013-2472-8 |
0.541 |
|
| 2013 |
Kumar S, Heister SD, Xu X, Salvador JR, Meisner GP. Thermoelectric generators for automotive waste heat recovery systems part I: Numerical modeling and baseline model analysis Journal of Electronic Materials. 42: 665-674. DOI: 10.1007/S11664-013-2471-9 |
0.546 |
|
| 2013 |
Shark SC, Zaseck CR, Graham JT, Pourpoint TL, Son SF, Heister SD. Visualization and performance of hybrid rocket solid fuels in an optical cylindrical combustor 49th Aiaa/Asme/Sae/Asee Joint Propulsion Conference. |
0.76 |
|
| 2013 |
Park KS, Heister SD. Numerical simulation of particle breakup/coalescence processes in shock waves 49th Aiaa/Asme/Sae/Asee Joint Propulsion Conference. |
0.406 |
|
| 2012 |
Ahn B, Ismailov M, Heister SD. Experimental study swirl injector dynamic response using a hydromechanical pulsator Journal of Propulsion and Power. 28: 585-595. DOI: 10.2514/1.B34261 |
0.766 |
|
| 2012 |
Dambach EM, Rankin BA, Pourpoint TL, Heister SD. Temperature estimations in the near-flame field resulting from hypergolic ignition using thin filament pyrometry Combustion Science and Technology. 184: 205-223. DOI: 10.1080/00102202.2011.627403 |
0.772 |
|
| 2012 |
Park KS, Heister SD. Agglomeration/breakup studies on radial slot flows in solid rocket motor 48th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2012. |
0.48 |
|
| 2011 |
Yoon C, Heister SD, Xia G, Merkle CL. Numerical modeling of injection of shear-thinning gel propellants through plain-orifice atomizer Journal of Propulsion and Power. 27: 944-954. DOI: 10.2514/1.B34135 |
0.634 |
|
| 2011 |
Ismailov M, Heister SD. Dynamic response of rocket swirl injectors, part II: Nonlinear dynamic response Journal of Propulsion and Power. 27: 412-421. DOI: 10.2514/1.B34045 |
0.757 |
|
| 2011 |
Ismailov M, Heister SD. Dynamic response of rocket swirl injectors, Part I: Wave reflection and resonance Journal of Propulsion and Power. 27: 402-411. DOI: 10.2514/1.B34044 |
0.747 |
|
| 2011 |
Tsohas J, Heister SD. Numerical simulations of liquid rocket coaxial injector hydrodynamics Journal of Propulsion and Power. 27: 793-810. DOI: 10.2514/1.47761 |
0.79 |
|
| 2011 |
Heister SD, Matsutomi Y, Bidadi S. Computational And Experimental Study Of Jet Interaction Fluidic Injectors Atomization and Sprays. 21: 127-138. DOI: 10.1615/Atomizspr.2011002751 |
0.769 |
|
| 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 |
0.364 |
|
| 2011 |
Park JJ, Lee MW, Yoon SS, Kim HY, James SC, Heister SD, Chandra S, Yoon WH, Park DS, Ryu J. Supersonic nozzle flow simulations for particle coating applications: Effects of shockwaves, nozzle geometry, ambient pressure, and substrate location upon flow characteristics Journal of Thermal Spray Technology. 20: 514-522. DOI: 10.1007/S11666-010-9542-8 |
0.356 |
|
| 2011 |
Trebs A, Slabaugh C, Lamont W, Heister SD, Meyer S. Gas turbine fuel system and combustion study with high temperature fuel injection 47th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2011. |
0.786 |
|
| 2011 |
Shark SC, Sippel TR, Son SF, Heister SD, Pourpoint TL. Theoretical performance analysis of metal hydride fuel additives for rocket propellant applications 47th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2011. |
0.767 |
|
| 2010 |
Park KS, Heister SD. Nonlinear modeling of drop size distributions produced by pressure-swirl atomizers International Journal of Multiphase Flow. 36: 1-12. DOI: 10.1016/J.Ijmultiphaseflow.2009.09.004 |
0.507 |
|
| 2010 |
Park KS, Heister SD. On the parallelization of unsteady BEM problems with variable mesh size Engineering Analysis With Boundary Elements. 34: 289-296. DOI: 10.1016/J.Enganabound.2009.09.004 |
0.404 |
|
| 2010 |
Dambach EM, Cho KY, Pourpoint TL, Heister SD. Ignition of advanced hypergolic propellants 46th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.743 |
|
| 2009 |
Herring NR, Heister SD. On the use of wire-coil inserts to augment tube heat transfer Journal of Enhanced Heat Transfer. 16: 19-34. DOI: 10.1615/Jenhheattransf.V16.I1.20 |
0.36 |
|
| 2009 |
Canino J, Heister SD. Contributions of orifice hydrodynamic instabilities to primary atomization Atomization and Sprays. 19: 91-102. DOI: 10.1615/Atomizspr.V19.I1.60 |
0.788 |
|
| 2009 |
Tsohas J, Appel B, Rettenmaier A, Walker M, Heister SD. Development and launch of the purdue hybrid rocket technology demonstrator 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.764 |
|
| 2009 |
Halsmer TI, Matsutomi Y, Heister SD. Flight performance comparison of pulse detonation and ramjet-propelled vehicles 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.79 |
|
| 2009 |
Sandroni AM, Cummings CB, Matsutomi Y, Meyer S, Heister SD. Biannular airbreathing nozzle rig facility development at Purdue University 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.784 |
|
| 2009 |
Tsohas J, Heister SD. CFD simulations of liquid rocket coaxial injector hydrodynamics 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.801 |
|
| 2009 |
Matsutomi Y, Heister SD. Studies on valveless pulse detonation engines 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.788 |
|
| 2008 |
Shimo M, Heister SD. Multicyclic-detonation-initiation studies in valveless pulsed detonation combustors Journal of Propulsion and Power. 24: 336-344. DOI: 10.2514/1.29546 |
0.373 |
|
| 2008 |
Shimo M, Heister SD. Schlieren visualization of multicyclic flame acceleration process in valveless pulsed detonation combustors Combustion Science and Technology. 180: 1613-1636. DOI: 10.1080/00102200802197403 |
0.375 |
|
| 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 |
0.427 |
|
| 2007 |
Macdonald ME, Canino JV, Heister SD. Nonlinear response of plain-orifice injectors to nonacoustic pressure oscillations Journal of Propulsion and Power. 23: 1204-1213. DOI: 10.2514/1.31189 |
0.785 |
|
| 2007 |
Corpening JH, Palmer RK, Heister SD, Rusek JJ. Combustion of advanced non-toxic hybrid propellants International Journal of Alternative Propulsion. 1: 154-173. DOI: 10.1504/Ijap.2007.013018 |
0.339 |
|
| 2007 |
Tsohas J, Canino JV, Heister SD. Computational modeling of rocket injector internal flows Collection of Technical Papers - 43rd Aiaa/Asme/Sae/Asee Joint Propulsion Conference. 6: 5508-5524. |
0.751 |
|
| 2007 |
Otterstatter MR, Meyer SE, Heister SD, Dambach EM. Design of an altitude-testing facility for lab-scale propulsion devices Collection of Technical Papers - 43rd Aiaa/Asme/Sae/Asee Joint Propulsion Conference. 4: 3186-3194. |
0.759 |
|
| 2007 |
Richardson R, Park H, Canino JV, Heister SD. Nonlinear dynamic response modeling of a swirl injector Collection of Technical Papers - 43rd Aiaa/Asme/Sae/Asee Joint Propulsion Conference. 5: 4322-4341. |
0.792 |
|
| 2006 |
Corpening JH, Heister SD, Anderson WE, Austin BJ. Thermal decomposition of hydrogen peroxide, part 2: Modeling studies Journal of Propulsion and Power. 22: 996-1005. DOI: 10.2514/1.13285 |
0.401 |
|
| 2006 |
Park H, Heister SD. Nonlinear simulation of free surfaces and atomization in pressure swirl atomizers Physics of Fluids. 18. DOI: 10.1063/1.2197876 |
0.463 |
|
| 2006 |
Park H, Yoon SS, Heister SD. On the nonlinear stability of a swirling liquid jet International Journal of Multiphase Flow. 32: 1100-1109. DOI: 10.1016/J.Ijmultiphaseflow.2006.05.002 |
0.455 |
|
| 2006 |
Park H, Heister SD. A numerical study of primary instability on viscous high-speed jets Computers and Fluids. 35: 1033-1045. DOI: 10.1016/J.Compfluid.2005.06.004 |
0.429 |
|
| 2006 |
Canino JV, Tsohas J, Sankaran V, Heister SD. Dynamic response of coaxial rocket injectors Collection of Technical Papers - Aiaa/Asme/Sae/Asee 42nd Joint Propulsion Conference. 5: 3850-3862. |
0.737 |
|
| 2006 |
MacDonald ME, Canino JV, Heister SD. Nonlinear response functions of drilled orifice injectors Collection of Technical Papers - Aiaa/Asme/Sae/Asee 42nd Joint Propulsion Conference. 5: 3833-3849. |
0.755 |
|
| 2005 |
Austin BL, Heister SD, Anderson WE. Characterization of pintle engine performance for nontoxic hypergolic bipropellants Journal of Propulsion and Power. 21: 627-635. DOI: 10.2514/1.7988 |
0.361 |
|
| 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 |
0.555 |
|
| 2005 |
Park H, Yoon SS, Heister SD. A nonlinear atomization model for computation of drop size distributions and spray simulations International Journal For Numerical Methods in Fluids. 48: 1219-1240. DOI: 10.1002/Fld.972 |
0.453 |
|
| 2005 |
Canino JV, Heister SD, Sankaran V, Zakharov SI. Unsteady response of recessed-post coaxial injectors 41st Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.768 |
|
| 2004 |
Kim BD, Heister SD. Two-phase modeling of hydrodynamic instabilities in coaxial injectors Journal of Propulsion and Power. 20: 468-479. DOI: 10.2514/1.10378 |
0.521 |
|
| 2004 |
Xu C, Heister SD, Blaisdell GA. Simulation Of Cavitated Flow In Orifices Fed By A Manifold Atomization and Sprays. 14: 37-52. DOI: 10.1615/Atomizspr.V14.I1.30 |
0.55 |
|
| 2004 |
Yoon SS, Heister SD. A nonlinear atomization model based on a boundary layer instability mechanism Physics of Fluids. 16: 47-61. DOI: 10.1063/1.1629301 |
0.351 |
|
| 2004 |
Yoon SS, Heister SD. A fully non-linear model for atomization of high-speed jets Engineering Analysis With Boundary Elements. 28: 345-357. DOI: 10.1016/S0955-7997(03)00083-3 |
0.356 |
|
| 2003 |
Matsutomi Y, Meyer SE, Heister SD. Impulse measurements and analytical studies on a cyclic pulse detonation engine 39th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.783 |
|
| 2002 |
Xu C, Heister SD, Field R. Modeling cavitating Venturi flows Journal of Propulsion and Power. 18: 1227-1234. DOI: 10.2514/2.6057 |
0.595 |
|
| 2002 |
Pham TL, Heister SD. Spray modeling using lagrangian droplet tracking in a homogeneous flow model Automization and Sprays: Journal of the International Institutions For Liquid Atomization and Spray Systems. 12: 687-707. DOI: 10.1615/Atomizspr.V12.I56.90 |
0.341 |
|
| 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 |
0.352 |
|
| 2002 |
Shimo M, Heister SD. Modeling oil flows on seal runners and engine sump walls 38th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. DOI: 10.1115/1.1924431 |
0.334 |
|
| 2002 |
Funk J, Heister SD, Rusek JJ. Reaction zones for impinging jets and sheets 38th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.545 |
|
| 2001 |
Xu C, Bunnell RA, Heister SD. On the influence of internal flow structure on performance of plain-orifice atomizers Atomization and Sprays. 11: 335-349. DOI: 10.1615/Atomizspr.V11.I4.30 |
0.541 |
|
| 2001 |
Yoon SS, Heister SD, Epperson JT, Sojka PE. Modeling multi-jet mode electrostatic atomization using boundary element methods Journal of Electrostatics. 50: 91-108. DOI: 10.1016/S0304-3886(00)00029-2 |
0.347 |
|
| 2000 |
Wernimont EJ, Heister SD. Combustion experiments in hydrogen peroxide/polyethylene hybrid rocket with catalytic ignition Journal of Propulsion and Power. 16: 318-327. DOI: 10.2514/2.5571 |
0.343 |
|
| 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 |
0.395 |
|
| 1999 |
Wernimont EJ, Heister SD. Reconstruction technique for reducing hybrid-rocket combustion test data Journal of Propulsion and Power. 15: 128-136. DOI: 10.2514/2.5401 |
0.314 |
|
| 1999 |
Bunnell RA, Heister SD, Yen C, Collicott SH. Cavitating injector flows: Validation of numerical models and simulations of pressure atomizers Automization and Sprays: Journal of the International Institutions For Liquid Atomization and Spray Systems. 9: 445-465. DOI: 10.1615/Atomizspr.V9.I5.10 |
0.358 |
|
| 1999 |
Moses MP, Collicott SH, Heister SD. Detection of aerodynamic effects in liquid jet breakup and droplet formation Automization and Sprays: Journal of the International Institutions For Liquid Atomization and Spray Systems. 9: 331-342. DOI: 10.1615/Atomizspr.V9.I4.10 |
0.316 |
|
| 1999 |
Murray IF, Heister SD. On a droplet's response to acoustic excitation International Journal of Multiphase Flow. 25: 531-550. DOI: 10.1016/S0301-9322(98)00051-2 |
0.35 |
|
| 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 |
0.382 |
|
| 1998 |
Caravella JR, Heister SD, Wernimont EJ. Characterization of fuel regression in a radial flow hybrid rocket Journal of Propulsion and Power. 14: 51-56. DOI: 10.2514/2.5265 |
0.421 |
|
| 1998 |
Hilbing JH, Heister SD. Nonlinear simulation of a high-speed, viscous liquid jet Atomization and Sprays. 8: 155-178. DOI: 10.1615/Atomizspr.V8.I2.20 |
0.346 |
|
| 1997 |
Heister SD. Boundary element methods for two-fluid free surface flows Engineering Analysis With Boundary Elements. 19: 309-317. DOI: 10.1016/S0955-7997(97)00037-4 |
0.357 |
|
| 1997 |
Setiawan ER, Heister SD. Nonlinear modeling of an infinite electrified jet Journal of Electrostatics. 42: 243-257. DOI: 10.1016/S0304-3886(97)00155-1 |
0.362 |
|
| 1996 |
Chen Y, Heister SD. Modeling cavitating flows in diesel injectors Atomization and Sprays. 6: 709-726. DOI: 10.1615/Atomizspr.V6.I6.50 |
0.402 |
|
| 1996 |
Chen Y, Heister SD. Modeling hydrodynamic nonequilibrium in cavitating flows Journal of Fluids Engineering, Transactions of the Asme. 118: 172-178. DOI: 10.1115/1.2817497 |
0.352 |
|
| 1996 |
Hilbing JH, Heister SD. Droplet size control in liquid jet breakup Physics of Fluids. 8: 1574-1581. DOI: 10.1063/1.868931 |
0.362 |
|
| 1995 |
Vonderwell DJ, Murray IF, Heister SD. Optimization of hybrid-rocket-booster fuel-grain design Journal of Spacecraft and Rockets. 32: 964-969. DOI: 10.2514/3.26716 |
0.391 |
|
| 1995 |
Heister SD, Rutz MW, Hilbing JA. Effect of acoustic perturbations on liquid jet atomization 31st Joint Propulsion Conference and Exhibit. DOI: 10.2514/2.5132 |
0.346 |
|
| 1995 |
Spangler CA, Hilbing JH, Heister SD. Nonlinear modeling of jet atomization in the wind-induced regime Physics of Fluids. 7: 964-971. DOI: 10.1063/1.868572 |
0.376 |
|
| 1995 |
Chen Y, Heister SD. Two-phase modeling of cavitated flows Computers and Fluids. 24: 799-809. DOI: 10.1016/0045-7930(95)00017-7 |
0.356 |
|
| 1994 |
Chen Y, Heister SD. A Numerical Treatment for Attached Cavitation Journal of Fluids Engineering-Transactions of the Asme. 116: 613-618. DOI: 10.1115/1.2910321 |
0.318 |
|
| 1990 |
Heister SD, Karagozian AR. Gaseous jet in supersonic crossflow Aiaa Journal. 28: 819-827. DOI: 10.2514/3.25125 |
0.607 |
|
| 1990 |
Heister SD, Karagozian AR. Vortex modeling of gaseous jets in a compressible crossflow Journal of Propulsion and Power. 6: 85-92. DOI: 10.2514/3.23227 |
0.61 |
|
| 1990 |
Heister SD, McDonough JM, Karagozian AR, Jenkins DW. Compressible vortex pair Journal of Fluid Mechanics. 220: 339-354. DOI: 10.1017/S0022112090003287 |
0.557 |
|
| 1990 |
Heister SD, McDonough JM, Karagozian AR, Jenkins DW. The compressible vortex pair . DOI: 10.1017/S0022112090003287 |
0.603 |
|
| 1989 |
Heister SD, Nguyen TT, Karagozian AR. Modeling of liquid jets injected transversely into a supersonic crossflow Aiaa Journal. 27: 1727-1734. DOI: 10.2514/3.10327 |
0.61 |
|
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