| Year |
Citation |
Score |
| 2021 |
Martinez A, Migliorino MT, Scalo C, Heister SD. Experimental and numerical investigation of standing-wave thermoacoustic instability under transcritical temperature conditions. The Journal of the Acoustical Society of America. 150: 2900. PMID 34717461 DOI: 10.1121/10.0006659 |
0.796 |
|
| 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 |
0.318 |
|
| 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 |
0.342 |
|
| 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 |
0.38 |
|
| 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 |
0.722 |
|
| 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 |
0.308 |
|
| 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 |
0.744 |
|
| 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 |
0.377 |
|
| 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 |
0.795 |
|
| 2016 |
Pfeil MA, Kulkarni AS, Ramachandran PV, Son SF, Heister SD. Solid amine-boranes as high-performance and hypergolic hybrid rocket fuels Journal of Propulsion and Power. 32: 23-31. DOI: 10.2514/1.B35591 |
0.527 |
|
| 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 |
0.63 |
|
| 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 |
0.566 |
|
| 2016 |
Cofer AG, O'Neill WJ, Heister SD, Cardiff EH, Alexeenko AA. Film-evaporation microthruster for cubesats Proceedings of the Ieee International Conference On Micro Electro Mechanical Systems (Mems). 2016: 1248-1251. DOI: 10.1109/MEMSYS.2016.7421864 |
0.538 |
|
| 2015 |
Pfeil MA, Dennis JD, Son SF, Heister SD, Pourpoint TL, Ramachandran PV. Characterization of ethylenediamine bisborane as a hypergolic hybrid rocket fuel additive Journal of Propulsion and Power. 31: 365-372. DOI: 10.2514/1.B35386 |
0.554 |
|
| 2015 |
Yazawa K, Heister SD, Fisher TS. Enhancement and optimization of planar impingement heat transfer for thermoelectric power generation Asme 2015 International Technical Conference and Exhibition On Packaging and Integration of Electronic and Photonic Microsystems, Interpack 2015, Collocated With the Asme 2015 13th International Conference On Nanochannels, Microchannels, and Minichannels. 1. DOI: 10.1115/IPACK2015-48692 |
0.546 |
|
| 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 |
0.677 |
|
| 2015 |
Wiest HK, Heister SD. Experimental study of a heated liquid jet in a crossflow 51st Aiaa/Sae/Asee Joint Propulsion Conference. |
0.574 |
|
| 2015 |
Kan BK, Heister SD. Characterization of injector response in a hypergolic pulse detonation rocket engine 51st Aiaa/Sae/Asee Joint Propulsion Conference. |
0.496 |
|
| 2015 |
Meier EJ, Heister SD. Influence of chamber geometry and operating conditions on the performance of feedback-free fluidic oscillators International Journal of Flow Control. 7: 19-36. |
0.552 |
|
| 2015 |
Meier EJ, Casiano MJ, Anderson WE, Heister SD. Investigation of combustion control in a dump combustor using the feedback free fluidic oscillator 51st Aiaa/Sae/Asee Joint Propulsion Conference. |
0.503 |
|
| 2014 |
Ramachandran PV, Kulkarni AS, Pfeil MA, Dennis JD, Willits JD, Heister SD, Son SF, Pourpoint TL. Amine-boranes: green hypergolic fuels with consistently low ignition delays. Chemistry (Weinheim An Der Bergstrasse, Germany). 20: 16869-72. PMID 25367843 DOI: 10.1002/Chem.201405224 |
0.76 |
|
| 2014 |
Hunt SA, Heister SD. Thermoacoustic oscillations in supercritical fuel flows 12th International Energy Conversion Engineering Conference, Iecec 2014. DOI: 10.2514/6.2014-3973 |
0.579 |
|
| 2014 |
Stechmann D, Lim D, Heister SD. Survey of rotating detonation wave combustor technology and potential rocket vehicle applications 50th Aiaa/Asme/Sae/Asee Joint Propulsion Conference 2014. DOI: 10.2514/6.2014-3902 |
0.533 |
|
| 2014 |
Kan BK, Heister SD. Chamber volume effects on hypergolic pulse detonation rocket engine 50th Aiaa/Asme/Sae/Asee Joint Propulsion Conference 2014. DOI: 10.2514/6.2014-3674 |
0.552 |
|
| 2014 |
Meier E, Heister SD. Computational characterization of the feedback free fluidic oscillator 50th Aiaa/Asme/Sae/Asee Joint Propulsion Conference 2014. DOI: 10.2514/6.2014-3583 |
0.476 |
|
| 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 |
0.771 |
|
| 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 |
0.753 |
|
| 2014 |
O'Neil PT, Heister SD. Evaluation of physical and ballistic properties of polymerized- dicyclopentadiene-based composite solid propellants Journal of Propulsion and Power. 30: 749-759. DOI: 10.2514/1.B34907 |
0.544 |
|
| 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 |
0.605 |
|
| 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 |
0.717 |
|
| 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 |
0.789 |
|
| 2013 |
O'Neil PT, Heister SD. Evaluation of processing and mechanical parameters of dicyclopentadiene- based gumstocks Journal of Propulsion and Power. 29: 1311-1322. DOI: 10.2514/1.B34848 |
0.546 |
|
| 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 |
0.58 |
|
| 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 |
0.793 |
|
| 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 |
0.725 |
|
| 2013 |
Trebs A, Heister SD. Improved injector metrics for supersonic combustors Journal of Propulsion and Power. 29: 274-275. DOI: 10.2514/1.B34589 |
0.779 |
|
| 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 |
0.64 |
|
| 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 |
0.671 |
|
| 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 |
0.679 |
|
| 2013 |
Park KS, Heister SD. Numerical simulation of particle breakup/coalescence processes in shock waves 49th Aiaa/Asme/Sae/Asee Joint Propulsion Conference. |
0.606 |
|
| 2013 |
Park J, Heister SD, Sullivan JP. Development of a counter-rotating vortex pair (CVP) mixer for aerospace applications 49th Aiaa/Asme/Sae/Asee Joint Propulsion Conference. |
0.557 |
|
| 2013 |
Sardeshmukh SV, Heister SD, Wang H, Sankaran V. Kinetics modeling of hypergolic propellants 49th Aiaa/Asme/Sae/Asee Joint Propulsion Conference. |
0.742 |
|
| 2013 |
Forness JM, Pourpoint TL, Heister SD. Experimental study of impingement and reaction of hypergolic droplets 49th Aiaa/Asme/Sae/Asee Joint Propulsion Conference. |
0.552 |
|
| 2013 |
Cofer AG, Heister SD, Alexeenko AA. Improved design and characterization of microNewton torsional balance thrust stand 49th Aiaa/Asme/Sae/Asee Joint Propulsion Conference. |
0.503 |
|
| 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. |
0.777 |
|
| 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. |
0.768 |
|
| 2012 |
Manship TD, Heister SD, O'Neil PT. Experimental investigation of high-burning-rate composite solid propellants Journal of Propulsion and Power. 28: 1389-1398. DOI: 10.2514/1.B34559 |
0.548 |
|
| 2012 |
Blank RA, Pourpoint TL, Meyer SE, Heister SD, Anderson WE. Experimental and theoretical performance of high-pressure hydrogen peroxide catalyst beds Journal of Propulsion and Power. 28: 912-917. DOI: 10.2514/1.B34432 |
0.565 |
|
| 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 |
0.803 |
|
| 2012 |
Kumar S, Heister SD, Xu X, Salvador JR, Meisner GP. Thermal design of thermoelectric generators for automobile waste heat recovery Asme 2012 Heat Transfer Summer Conf. Collocated With the Asme 2012 Fluids Engineering Div. Summer Meeting and the Asme 2012 10th Int. Conf. On Nanochannels, Microchannels and Minichannels, Ht 2012. 1: 67-77. DOI: 10.1115/HT2012-58129 |
0.466 |
|
| 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 |
0.786 |
|
| 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. |
0.657 |
|
| 2012 |
O'Neil PT, Heister SD. Evaluation of ballistic and mechanical properties of polymerized-dicyclopentadiene-based composite solid propellants 48th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2012. |
0.459 |
|
| 2012 |
O'Neil PT, Heister SD. Investigation of the effect of gelling agents on dicyclopentadiene's rheological characteristics for improvement of composite solid propellant quality 48th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2012. |
0.455 |
|
| 2012 |
O'Neil PT, Heister SD. Experimental evaluation of processing and aging characteristics of polymerized dicyclopentadiene for use as a composite solid propellant binder 48th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2012. |
0.466 |
|
| 2012 |
Yoon C, Heister SD, Campanella OE. Plain-orifice gelled propellant flow characteristics with rheological hysteresis 48th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2012. |
0.573 |
|
| 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. |
0.776 |
|
| 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 |
0.734 |
|
| 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 |
0.794 |
|
| 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 |
0.791 |
|
| 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 |
0.801 |
|
| 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 |
0.776 |
|
| 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 |
0.611 |
|
| 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 |
0.601 |
|
| 2011 |
Rettenmaier AK, Heister SD. Experimental evaluation of erosive burning in a planar combustor 47th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2011. |
0.537 |
|
| 2011 |
Hinkelman MC, Heister SD, Austin BL. Evaluation of solid composite propellants using a dicyclopentadiene binder 47th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2011. |
0.501 |
|
| 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. |
0.794 |
|
| 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. |
0.775 |
|
| 2011 |
Yoon C, Heister SD, Sojka PE, Watson CC, Xia G, Merkle CL. Injector flow characteristics for gel propellants 47th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2011. |
0.572 |
|
| 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 |
0.66 |
|
| 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 |
0.6 |
|
| 2010 |
Park KS, Xia G, Heister SD. Modeling two-phase flow with stochastic coalescence/breakage model 46th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.554 |
|
| 2010 |
Dambach EM, Cho KY, Pourpoint TL, Heister SD. Ignition of advanced hypergolic propellants 46th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.754 |
|
| 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 |
0.603 |
|
| 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 |
0.794 |
|
| 2009 |
Ismailov M, Heister SD. Nonlinear modeling of classical swirl injector dynamics 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.517 |
|
| 2009 |
Tsohas J, Heister SD. CFD simulations of liquid rocket coaxial injector hydrodynamics 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.81 |
|
| 2009 |
Matsutomi Y, Heister SD. Studies on valveless pulse detonation engines 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.802 |
|
| 2009 |
Ahn B, Ismailov M, Heister SD. Forced excitation of swirl injectors using a hydro-mechanical pulsator 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.576 |
|
| 2009 |
Slaby JM, Moss J, Heister SD. Experimental program to assess erosive burning in segmented solid rocket motors 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.528 |
|
| 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. |
0.8 |
|
| 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. |
0.773 |
|
| 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. |
0.796 |
|
| 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 |
0.607 |
|
| 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 |
0.608 |
|
| 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 |
0.631 |
|
| 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 |
0.79 |
|
| 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 |
0.584 |
|
| 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. |
0.772 |
|
| 2007 |
Rodkey SC, Heister SD, Collicott SH. Physics of gas turbine engine bearing chambers Collection of Technical Papers - 43rd Aiaa/Asme/Sae/Asee Joint Propulsion Conference. 1: 282-296. |
0.522 |
|
| 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. |
0.769 |
|
| 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. |
0.8 |
|
| 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 |
0.628 |
|
| 2006 |
Herring NR, Heister SD. Review of the development of compact, high performance heat exchangers for gas turbine applications American Society of Mechanical Engineers, Heat Transfer Division, (Publication) Htd. DOI: 10.1115/IMECE2006-14920 |
0.535 |
|
| 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 |
0.647 |
|
| 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 |
0.64 |
|
| 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 |
0.625 |
|
| 2006 |
Kim BD, Heister SD. Numerical modeling of hydrodynamic instability of swirl coaxial injector in a recessed region Collection of Technical Papers - Aiaa/Asme/Sae/Asee 42nd Joint Propulsion Conference. 5: 3953-3966. |
0.563 |
|
| 2006 |
Zakharov SI, Richardson R, Heister SD. Hydrodynamic modeling of swirl injectors with multiple rows of tangential channels Collection of Technical Papers - Aiaa/Asme/Sae/Asee 42nd Joint Propulsion Conference. 11: 8418-8430. |
0.522 |
|
| 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. |
0.752 |
|
| 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. |
0.759 |
|
| 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 |
0.598 |
|
| 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 |
0.7 |
|
| 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 |
0.641 |
|
| 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 |
0.678 |
|
| 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 |
0.555 |
|
| 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 |
0.596 |
|
| 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 |
0.602 |
|
| 2004 |
Chao CC, Heister SD. Contributions of atomization to F-1 engine combustion instabilities Engineering Analysis With Boundary Elements. 28: 1045-1053. DOI: 10.1016/j.enganabound.2004.04.003 |
0.556 |
|
| 2004 |
Yoon SS, Heister SD. Analytical formulas for the velocity field induced by an infinitely thin vortex ring International Journal For Numerical Methods in Fluids. 44: 665-672. DOI: 10.1002/Fld.666 |
0.54 |
|
| 2004 |
Kim BD, Heister SD. Effect of chamber pressure variation on high-frequency hydrodynamic instability of shear coaxial injector 40th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.512 |
|
| 2004 |
Xu C, Heister SD, Blaisdell GA. Simulation of cavitated flow in orifices FED by a manifold Atomization and Sprays. 14: 37-52. |
0.57 |
|
| 2004 |
Corpening JH, Heister SD, Anderson WE, Austin BJ. A model for thermal decomposition of hydrogen peroxide 40th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.585 |
|
| 2004 |
Heister SD, Meyer SE, Anderson WE, Hrbud I, Merkle CL. Propulsion educational programs and facilities at purdue university 40th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.43 |
|
| 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. |
0.795 |
|
| 2003 |
Xu C, Heister SD, Fields R. Cavitating flow modeling including energy interchange effects 39th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.571 |
|
| 2003 |
Ji J, Shimo M, Heister SD, Gore JP. Combustion diagnostics of the cyclic pulse detonation process with infrared spectroscopy 39th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.554 |
|
| 2002 |
Xu C, Heister SD, Field R. Modeling cavitating Venturi flows Journal of Propulsion and Power. 18: 1227-1234. DOI: 10.2514/2.6057 |
0.709 |
|
| 2002 |
Mailhe LM, Heister SD. Design of a hybrid chemical/electric propulsion orbital transfer vehicle Journal of Spacecraft and Rockets. 39: 131-139. DOI: 10.2514/2.3791 |
0.544 |
|
| 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 |
0.593 |
|
| 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 |
0.602 |
|
| 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 |
0.588 |
|
| 2002 |
Heister SD, Rusek JJ. Development of a design/build/test course in rocket propulsion 38th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.496 |
|
| 2002 |
Kim B, Heister SD. Two-phase modeling and hydrodynamic instability study of shear coaxial injector flow 38th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.536 |
|
| 2002 |
Bulathsinghala I, Kowalkowski M, Heister SD. Propulsion for agile landmines II, dynamic simulations and experiments 38th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.536 |
|
| 2002 |
Kowalkowski M, Bulathsinghala I, Heister SD. Trajectory control of agile landmines I 38th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.503 |
|
| 2002 |
Funk J, Heister SD, Rusek JJ. Reaction zones for impinging jets and sheets 38th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.678 |
|
| 2002 |
Beutien TR, Heister SD, Rusek JJ, Meyer S. Cordierite-based catalytic beds for 98% hydrogen peroxide 38th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.497 |
|
| 2002 |
Remson AE, Crossley WA, Heister SD, McMillin JE. Consumable satellite structures for apogee insertion applications 38th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.496 |
|
| 2002 |
Miller KJ, Martin TN, Edwards JM, Heister SD, Meyer SE. Immersion test apparatus for studying monopropellant decomposition with various catalysts 38th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.484 |
|
| 2002 |
Shimo M, Meyer SE, Heister SD, Weng CS, Ji J, Gore JP. An experimental and computational study of pulsed detonations in a single tube 38th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.56 |
|
| 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 |
0.669 |
|
| 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 |
0.593 |
|
| 2001 |
Heister SD. Simulating two-phase flows inside high-speed injectors Advances in Fluid Mechanics. 29: 253-263. |
0.555 |
|
| 2001 |
Xu C, Blaisdell GA, Heister SD. Simulations of turbulent, cavitating flows in an injector slot/orifice Advances in Fluid Mechanics. 29: 185-195. |
0.585 |
|
| 2001 |
Yoon SS, Pham TL, Heister SD. Development of a fully coupled injection/atomization code Advances in Fluid Mechanics. 29: 265-273. |
0.55 |
|
| 2001 |
Lim KH, Brodrecht DJ, Heister SD, Rusek JJ. Alloying effects in an aluminum-hydrogen peroxide semi-fuel cell European Space Agency, (Special Publication) Esa Sp. 353-358. |
0.497 |
|
| 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 |
0.588 |
|
| 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 |
0.626 |
|
| 2000 |
Yoon SS, Heister SD. Analytic solution for fluxes at interior points for the 2D Laplace equation Engineering Analysis With Boundary Elements. 24: 155-160. DOI: 10.1016/S0955-7997(99)00059-4 |
0.557 |
|
| 2000 |
Schoonover PL, Crossley WA, Heister SD. Application of a genetic algorithm to the optimization of hybrid rockets Journal of Spacecraft and Rockets. 37: 622-629. |
0.473 |
|
| 2000 |
Frolik SA, Austin BL, Rusek JJ, Heister SD. Development of hypergoiic liquid fuels for use with hydrogen peroxide 35th Intersociety Energy Conversion Engineering Conference and Exhibit. |
0.533 |
|
| 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 |
0.573 |
|
| 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 |
0.605 |
|
| 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 |
0.573 |
|
| 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 |
0.59 |
|
| 1999 |
Yoon SS, Heister SD. Simulation of the nonlinear dynamics of charged liquids using boundary element methods Boundary Element Technology Xiii. Proceedings of the 1999 Thirteenth International Conference On Boundary Element Technology, Betech '99. 13-24. |
0.523 |
|
| 1999 |
Funk JE, Heister SD, Humble R, Purcell N. Development testing of non-toxic, storable hypergolic liquid propellants 35th Joint Propulsion Conference and Exhibit. |
0.532 |
|
| 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 |
0.624 |
|
| 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 |
0.637 |
|
| 1998 |
Schoonover PL, Crossley WA, Heister SD. Application of genetic algorithms to the optimization of hybrid rockets 34th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. DOI: 10.2514/2.3610 |
0.538 |
|
| 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 |
0.59 |
|
| 1998 |
Heister SD. Modeling primary atomization processes 34th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.547 |
|
| 1998 |
Vandenboom M, Heister SD. Application of advanced materials in a composite rocket nozzle 34th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.501 |
|
| 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 |
0.607 |
|
| 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 |
0.598 |
|
| 1997 |
Heister SD. Modeling atomization processes Proceedings of the Industrial Waste Conference. 511-523. |
0.535 |
|
| 1997 |
Wernimont EJ, Heister SD. Experimental study of chamber pressure effects in hydrogen peroxide oxidized hybrid rockets 33rd Joint Propulsion Conference and Exhibit. |
0.572 |
|
| 1997 |
Rump KM, Heister SD. Modeling the effect of unsteady chamber condtions on atomization processes 33rd Joint Propulsion Conference and Exhibit. |
0.598 |
|
| 1996 |
Chen Y, Heister SD. Modeling cavitating flows in diesel injectors Atomization and Sprays. 6: 709-726. DOI: 10.1615/Atomizspr.V6.I6.50 |
0.631 |
|
| 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 |
0.601 |
|
| 1996 |
Hilbing JH, Heister SD. Droplet size control in liquid jet breakup Physics of Fluids. 8: 1574-1581. DOI: 10.1063/1.868931 |
0.601 |
|
| 1996 |
Heister SD, Messersmith NL. Launch competition for rocket propulsion education International Journal of Engineering Education. 12: 229-238. |
0.466 |
|
| 1996 |
Wernimont EJ, Heister SD. Progress in hydrogen peroxide oxidized hybrid rocket experiments 32nd Joint Propulsion Conference and Exhibit. |
0.575 |
|
| 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 |
0.615 |
|
| 1995 |
Hejl RJ, Heister SD. Solid rocket motor grain burnback analysis using adaptive grids Journal of Propulsion and Power. 11: 1006-1011. DOI: 10.2514/3.23930 |
0.531 |
|
| 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 |
0.596 |
|
| 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 |
0.611 |
|
| 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 |
0.602 |
|
| 1995 |
Wernimont EJ, Heister SD. Characterization of fuel regression in hybrid rockets utilizing hydrogen peroxide oxidizer 31st Joint Propulsion Conference and Exhibit. |
0.545 |
|
| 1994 |
Osborn JR, Heister SD. Solid rocket motor temperature sensitivity Journal of Propulsion and Power. 10: 908-910. DOI: 10.2514/3.23831 |
0.532 |
|
| 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 |
0.327 |
|
| 1993 |
Heister SD. Ballistics of solid rocket motors with spatial burning rate variations Journal of Propulsion and Power. 9: 649-651. DOI: 10.2514/3.23671 |
0.546 |
|
| 1992 |
Heister SD, Davis RJ. Predicting burning time variations in solid rocket motors Journal of Propulsion and Power. 8: 564-569. DOI: 10.2514/3.23515 |
0.542 |
|
| 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 |
0.608 |
|
| 1990 |
Heister SD, McDonough JM, Karagozian AR, Jenkins DW. The compressible vortex pair . DOI: 10.1017/S0022112090003287 |
0.609 |
|
| 1990 |
Heister SD, McDonough JM, Karagozian AR, Jenkins DW. Compressible vortex pair Journal of Fluid Mechanics. 220: 339-354. DOI: 10.1017/S0022112090003287 |
0.558 |
|
| 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 |
0.612 |
|
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