| Year |
Citation |
Score |
| 2017 |
DeSouza S, Segal C. Sub- and supercritical jet disintegration Physics of Fluids. 29: 047107. DOI: 10.1063/1.4979486 |
0.46 |
|
| 2016 |
Barnes FW, Tu Q, Segal C. Fuel-air mixing experiments in a directly fueled supersonic cavity flameholder Journal of Propulsion and Power. 32: 305-310. DOI: 10.2514/1.B35701 |
0.757 |
|
| 2015 |
Barnes FW, Segal C. Cavity-based flameholding for chemically-reacting supersonic flows Progress in Aerospace Sciences. 76: 24-41. DOI: 10.1016/J.Paerosci.2015.04.002 |
0.739 |
|
| 2014 |
Barnes FW, Tu Q, Segal C. Mixing and mass exchange for cavities in supersonic flows Aiaa Aviation 2014 -19th Aiaa International Space Planes and Hypersonic Systems and Technologies Conference. |
0.388 |
|
| 2013 |
Roy A, Segal C, Joly C. Spreading angle and core length analysis of supercritical jets Aiaa Journal. 51: 2009-2014. DOI: 10.2514/1.J052415 |
0.404 |
|
| 2013 |
Kelly S, Segal C. Characteristics of thermal cavitation on a two-dimensional hydrofoil Journal of Propulsion and Power. 29: 410-416. DOI: 10.2514/1.B34707 |
0.486 |
|
| 2013 |
Roy A, Joly C, Segal C. Disintegrating supercritical jets in a subcritical environment Journal of Fluid Mechanics. 717: 193-202. DOI: 10.1017/Jfm.2012.566 |
0.476 |
|
| 2012 |
Roy A, Segal C. Linear stability analysis of a sub-to-supercritical jet Physics of Fluids. 24. DOI: 10.1063/1.3694806 |
0.387 |
|
| 2012 |
Roy A, Segal C, Joly C. Supercritical fuel injection in multi-species systems 48th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2012. |
0.331 |
|
| 2012 |
Kelly S, Segal C. Experiments in thermosensitive cavitation of a cryogenic rocket propellant surrogate 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.335 |
|
| 2011 |
Roy A, Gustavsson JPR, Segal C. Spectroscopic properties of a perfluorinated ketone for PLIF applications Experiments in Fluids. 51: 1455-1463. DOI: 10.1007/S00348-011-1163-6 |
0.343 |
|
| 2010 |
Kelly S, Segal C. Simulation of cryogenics cavitation 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.2514/1.J051033 |
0.421 |
|
| 2010 |
Roy A, Segal C. Experimental study of fluid jet mixing at supercritical conditions Journal of Propulsion and Power. 26: 1205-1211. DOI: 10.2514/1.48462 |
0.445 |
|
| 2010 |
Tu Q, Takahashi H, Segal C. Effects of pylon-aided fuel injection on mixing in a supersonic flowfield 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.2514/1.48393 |
0.653 |
|
| 2010 |
Vaidyanathan A, Gustavsson J, Segal C. One-and three-dimensional wall heat flux calculations in a O 2/H2 system Journal of Propulsion and Power. 26: 186-188. DOI: 10.2514/1.44640 |
0.733 |
|
| 2010 |
Roy A, Segal C. Sub-to-Supercritical jet mixing and core length analysis 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.314 |
|
| 2009 |
Tu Q, Segal C. Isolator/combustion chamber interactions during supersonic combustion 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. DOI: 10.2514/1.46156 |
0.659 |
|
| 2009 |
Vaidyanathan A, Gustavsson J, Segal C. Oxygen/hydrogen-planar-laser-induced fluorescence measurements and accuracy investigation in high-pressure combustion Journal of Propulsion and Power. 25: 864-874. DOI: 10.2514/1.39013 |
0.755 |
|
| 2009 |
Gustavsson JPR, Denning KC, Segal C, Dorney DJ. Incipient cavitation studied under strong thermodynamic effect Aiaa Journal. 47: 710-716. DOI: 10.2514/1.38987 |
0.372 |
|
| 2009 |
Roy A, Segal C. Experimental study of subcritical to supercritical jet mixing 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.1615/Intjenergeticmaterialschemprop.V8.I3.50 |
0.452 |
|
| 2008 |
Thakur A, Segal C. Concentration distribution in a supersonic flow recirculation region Journal of Propulsion and Power. 24: 64-73. DOI: 10.2514/1.25396 |
0.741 |
|
| 2008 |
Gustavsson JPR, Denning KC, Segal C. Hydrofoil cavitation under strong thermodynamic effect Journal of Fluids Engineering, Transactions of the Asme. 130: 0913031-0913035. DOI: 10.1115/1.2953297 |
0.431 |
|
| 2008 |
Segal C, Polikhov SA. Subcritical to supercritical mixing Physics of Fluids. 20. DOI: 10.1063/1.2912055 |
0.629 |
|
| 2008 |
Gustavsson JPR, Denning K, Segal C. Experimental study of cryogenic cavitation using fluoroketone 46th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.316 |
|
| 2007 |
Gustavsson JP, Segal C. Fluorescence spectrum of 2-trifluoromethyl-1,1,1,2,4,4,5,5,5-nonafluoro-3-pentanone. Applied Spectroscopy. 61: 903-7. PMID 17716411 DOI: 10.1366/000370207781540088 |
0.65 |
|
| 2007 |
Conley A, Vaidyanathan A, Segal C. Heat flux measurements for a GO2/GH2 single-element, shear injector Journal of Spacecraft and Rockets. 44: 633-639. DOI: 10.2514/1.26678 |
0.772 |
|
| 2007 |
Vinogradov VA, Shikhman YM, Segal C. A review of fuel pre-injection in supersonic, chemically reacting flows Applied Mechanics Reviews. 60: 139-148. DOI: 10.1115/1.2750346 |
0.492 |
|
| 2007 |
Vaidyanathan A, Gustavsson J, Segal C. Heat fluxes/OH PLIF measurements in a GO2/GH2 single-element, shear injector Collection of Technical Papers - 43rd Aiaa/Asme/Sae/Asee Joint Propulsion Conference. 6: 5726-5743. |
0.346 |
|
| 2006 |
Portz R, Segal C. Penetration of gaseous jets in supersonic flows Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 20: 14933-14946. DOI: 10.2514/1.23541 |
0.432 |
|
| 2006 |
Nori V, Lerma N, Gustavsson J, Segal C, Fernandez R. Forced oscillations in a mixed-compression inlet at Mach 3.5 for pulse detonation engine systems Journal of Fluids Engineering, Transactions of the Asme. 128: 494-506. DOI: 10.1115/1.2174061 |
0.709 |
|
| 2006 |
Gustavsson JPR, Segal C, Dolbier WR, Ameduri B, Kostov G. Combustion and thermal decomposition of fluorinated polymers Combustion Science and Technology. 178: 2097-2114. DOI: 10.1080/00102200600860681 |
0.34 |
|
| 2006 |
Conley A, Vaidyanathan A, Segal C. Heat fluxes measurements in a GO2/GH2 single-element, shear injector Collection of Technical Papers - Aiaa/Asme/Sae/Asee 42nd Joint Propulsion Conference. 9: 7011-7024. |
0.43 |
|
| 2006 |
Thakur A, Segal C. Analyses of non-premixed flameholding behind a step in supersonic flow Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 22: 16597-16613. |
0.725 |
|
| 2006 |
Vinogradov VA, Shikhman YM, Segal C. Review of fuel pre-injection studies in a high speed airflow Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 16: 12357-12370. |
0.401 |
|
| 2006 |
Polikhov SA, Segal C. Two phase flow supercritical mixing Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 12: 9149-9158. |
0.343 |
|
| 2005 |
Gustavsson JPR, Segal C. Filtered Rayleigh scattering velocimetry-accuracy investigation in a M=2.2 axisymmetric jet Experiments in Fluids. 38: 11-20. DOI: 10.1007/S00348-004-0867-2 |
0.345 |
|
| 2005 |
Thakur A, Segal C. Flameholding in supersonic flow - Non-premixed recirculation region composition A Collection of Technical Papers - 13th Aiaa/Cira International Space Planes and Hypersonic Systems and Technologies Conference. 3: 1615-1628. |
0.699 |
|
| 2004 |
Portz R, Segal C. Mixing in high-speed flows with thick boundary layers 40th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.302 |
|
| 2003 |
Mikolaitis DW, Segal C, Chandy A. Ignition delay for jet propellant 10/air and jet propellant 10/high-energy density fuel/air mixtures Journal of Propulsion and Power. 19: 601-606. DOI: 10.2514/2.6147 |
0.405 |
|
| 2003 |
Gustavsson J, Nori V, Segal C. Inlet/engine interactions in an axisymmetric pulse detonation engine system Journal of Propulsion and Power. 19: 282-286. DOI: 10.2514/2.6109 |
0.703 |
|
| 2003 |
Mullagiri S, Segal C, Hubner PJ. Oscillating flows in a model pulse detonation engine inlet Aiaa Journal. 41: 324-326. DOI: 10.2514/2.1951 |
0.413 |
|
| 2003 |
Thakur A, Segal C. Flameholding analyses in supersonic flow 12th Aiaa International Space Planes and Hypersonic Systems and Technologies. |
0.704 |
|
| 2003 |
Nori V, Lerma N, Segal C, Femandez R. Oscillating flows in inlets for pulsed detonation engines 41st Aerospace Sciences Meeting and Exhibit. |
0.403 |
|
| 2001 |
Owens MG, Mullagiri S, Segal C, Ortwerth PJ, Mathur AB. Thermal choking analyses in a supersonic combustor Journal of Propulsion and Power. 17: 611-616. DOI: 10.2514/2.5785 |
0.473 |
|
| 2001 |
Owens M, Mullagiri S, Segal C, Vinogradov VA. Effects of fuel preinjection on mixing in Mach 1.6 airflow Journal of Propulsion and Power. 17: 605-610. DOI: 10.2514/2.5784 |
0.527 |
|
| 2001 |
Segal C, Pethe S, Williams KR. Combustion of high-energy-high-density fuels Combustion Science and Technology. 163: 229-244. DOI: 10.1080/00102200108952157 |
0.373 |
|
| 2001 |
Owens M, Segal C. Development of a hybrid-fuzzy air temperature controller for a supersonic combustion test facility Experiments in Fluids. 31: 26-33. DOI: 10.1007/S003480000255 |
0.329 |
|
| 2001 |
Mullagiri S, Segal C. Oscillating flows in inlets of pulse detonation engines 39th Aerospace Sciences Meeting and Exhibit. |
0.325 |
|
| 2000 |
Livingston T, Segal C, Schindler M, Vinogradov VA. Penetration and spreading of liquid jets in an external-internal compression inlet Aiaa Journal. 38: 989-994. DOI: 10.2514/2.1082 |
0.499 |
|
| 1999 |
Ebert M, Shyy W, Thakur S, Segal C, Liou MS. Heat transfer and fluid flow in rotating cavities 37th Aerospace Sciences Meeting and Exhibit. |
0.31 |
|
| 1999 |
Vinogradov VA, Owens M, Mullagiri S, Segal C. Effects of fuel pre-injection on mixing in a Mach 1.6 airflow 9th International Space Planes and Hypersonic Systems and Technologies Conference. 1-9. |
0.442 |
|
| 1998 |
Daines R, Segal C. Combined rocket and airbreathing propulsion systems for space-launch applications Journal of Propulsion and Power. 14: 605-612. DOI: 10.2514/2.5352 |
0.326 |
|
| 1998 |
Pethe S, Livingston T, Segal C, Williams KR, Powell DH. Physico-chemical properties and combustion characteristics of new high-energy-density caged hydrocarbon compounds Combustion Science and Technology. 132: 17-35. DOI: 10.1080/00102209808952009 |
0.357 |
|
| 1998 |
Abate G, Shyy W, Segal C, Anderson C. Gas dynamic structure of a shock wave undergoing sudden expansion 20th Aiaa Advanced Measurement and Ground Testing Technology Conference. |
0.327 |
|
| 1998 |
Owens MG, Tehranian S, Segal C, Vinogradov VA. Flame-holding configurations for kerosene combustion in a Mach 1.8 airflow Journal of Propulsion and Power. 14: 456-461. |
0.407 |
|
| 1997 |
Segal C, Owens MG, Tehranian S, Vinogradov V. Flameholding configurations for kerosene combustion in a mach 1.8 airflow 33rd Joint Propulsion Conference and Exhibit. DOI: 10.2514/2.5322 |
0.494 |
|
| 1997 |
Owens M, Segal C, Auslender AH. Effects of mixing schemes on kerosene combustion in a supersonic airstream Journal of Propulsion and Power. 13: 525-531. DOI: 10.2514/2.5198 |
0.508 |
|
| 1997 |
Segal C, Friedauer MJ, Udaykumar HS, Shyy W, Marchand AP. Ignition characteristics of a new high-energy density fuel in high-speed flows Journal of Propulsion and Power. 13: 246-249. DOI: 10.2514/2.5155 |
0.493 |
|
| 1997 |
Segal C. Aircraft engine bay cooling and ventilation: Design and modeling Journal of Aircraft. 34: 141-144. DOI: 10.2514/2.2150 |
0.446 |
|
| 1997 |
Udaykumar HS, Shyy W, Segal C, Pal S. Phase change characteristics of energetic solid fuels in turbulent reacting flows Numerical Heat Transfer; Part a: Applications. 32: 97-109. DOI: 10.1080/10407789708913882 |
0.465 |
|
| 1996 |
Segal C, Shyy W. Energetic fuels for combustion applications Journal of Energy Resources Technology, Transactions of the Asme. 118: 180-186. DOI: 10.1115/1.2793860 |
0.407 |
|
| 1996 |
Segal C, Young CD. Development of an experimentally flexible facility for mixing-combustion interactions in supersonic flow Journal of Energy Resources Technology, Transactions of the Asme. 118: 152-158. DOI: 10.1115/1.2792707 |
0.464 |
|
| 1996 |
Owens M, Segal C. Combustion of kerosene in a supersonic airstream thermal efficiency of selected injection configurations 32nd Joint Propulsion Conference and Exhibit. 1-9. |
0.407 |
|
| 1996 |
Segal C, Friedauer MJ, Udaykumar HS, Shyy W. Combustion characteristics of high-energy/high-density hydrocarbon compounds American Society of Mechanical Engineers, Heat Transfer Division, (Publication) Htd. 335: 353-359. |
0.393 |
|
| 1995 |
Segal C, McDaniel JC, Whitehurst RB, Krauss RH. Mixing and Chemical Kinetics Interactions in a Mach 2 Reacting Flow Journal of Propulsion and Power. 11: 308-314. DOI: 10.2514/3.51426 |
0.538 |
|
| 1995 |
Segal C, Haj-Hariri H, McDaniel JC. Effects of chemical reaction model on calculations of supersonic combustion flows Journal of Propulsion and Power. 11: 565-568. DOI: 10.2514/3.23879 |
0.347 |
|
| 1995 |
Bonghi L, Dunlap MJ, Owens M, Young C, Segal C. Hydrogen piloted energy for supersonic combustion of liquid fuels 33rd Aerospace Sciences Meeting and Exhibit. |
0.39 |
|
| 1993 |
Abbitt JD, Segal C, McDaniel JC, Krauss RH, Whitehurst RB. Experimental supersonic hydrogen combustion employing staged injection behind a rearward-facing step Journal of Propulsion and Power. 9: 472-478. DOI: 10.2514/3.23646 |
0.512 |
|
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