Year |
Citation |
Score |
2020 |
Gena AW, Voelker C, Settles GS. Qualitative and quantitative schlieren optical measurement of the human thermal plume. Indoor Air. PMID 32302432 DOI: 10.1111/Ina.12674 |
0.333 |
|
2016 |
Settles GS, Fulghum MR. The Focusing Laser Differential Interferometer, an Instrument for Localized Turbulence Measurements in Refractive Flows Journal of Fluids Engineering, Transactions of the Asme. 138. DOI: 10.1115/1.4033960 |
0.743 |
|
2014 |
Craven BA, Hargather MJ, Volpe JA, Frymire SP, Settles GS. Design of a high-throughput chemical trace detection portal that samples the aerodynamic wake of a walking person Ieee Sensors Journal. 14: 1852-1866. DOI: 10.1109/Jsen.2014.2304538 |
0.43 |
|
2013 |
Hargather MJ, Settles GS, Gogineni S. Optical diagnostics for characterizing a transitional shear layer over a supersonic cavity Aiaa Journal. 51: 2977-2982. DOI: 10.2514/1.J052421 |
0.391 |
|
2013 |
Fulghum MR, Hargather MJ, Settles GS. Integrated impactor/detector for a high-throughput explosive-trace detection portal Ieee Sensors Journal. 13: 1252-1258. DOI: 10.1109/Jsen.2012.2231671 |
0.724 |
|
2013 |
Young RM, Hargather MJ, Settles GS. Shear stress and particle removal measurements of a round turbulent air jet impinging normally upon a planar wall Journal of Aerosol Science. 62: 15-25. DOI: 10.1016/J.Jaerosci.2013.04.002 |
0.325 |
|
2012 |
Hargather MJ, Settles GS. A comparison of three quantitative schlieren techniques Optics and Lasers in Engineering. 50: 8-17. DOI: 10.1016/J.Optlaseng.2011.05.012 |
0.341 |
|
2012 |
Svingala FR, Hargather MJ, Settles GS. Optical techniques for measuring the shock Hugoniot using ballistic projectile and high-explosive shock initiation International Journal of Impact Engineering. 50: 76-82. DOI: 10.1016/J.Ijimpeng.2012.08.006 |
0.762 |
|
2012 |
Grujicic M, He T, Pandurangan B, Svingala FR, Settles GS, Hargather MJ. Experimental characterization and material-model development for microphase-segregated polyurea: An overview Journal of Materials Engineering and Performance. 21: 2-16. DOI: 10.1007/S11665-011-9875-6 |
0.749 |
|
2011 |
Hargather MJ, Lawson MJ, Settles GS, Weinstein LM. Seedless velocimetry measurements by schlieren image velocimetry Aiaa Journal. 49: 611-620. DOI: 10.2514/1.J050753 |
0.407 |
|
2011 |
Hargather MJ, Staymates ME, Madalis MJ, Smith DJ, Settles GS. The internal aerodynamics of cargo containers for trace chemical sampling and detection Ieee Sensors Journal. 11: 1184-1193. DOI: 10.1109/Jsen.2010.2087747 |
0.357 |
|
2011 |
Hargather MJ, Settles GS. Background-oriented schlieren visualization of heating and ventilation flows: HVAC-BOS Hvac and R Research. 17: 771-780. DOI: 10.1080/10789669.2011.588985 |
0.301 |
|
2010 |
Hargather MJ, Settles GS. Natural-background-oriented schlieren imaging Experiments in Fluids. 48: 59-68. DOI: 10.1007/S00348-009-0709-3 |
0.327 |
|
2010 |
Hargather MJ, Settles GS, Madalis MJ. Schlieren imaging of loud sounds and weak shock waves in air near the limit of visibility Shock Waves. 20: 9-17. DOI: 10.1007/S00193-009-0226-6 |
0.359 |
|
2010 |
Biss MM, Settles GS. On the use of composite charges to determine insensitive explosive material properties at the laboratory scale Propellants, Explosives, Pyrotechnics. 35: 452-460. DOI: 10.1002/Prep.200900070 |
0.756 |
|
2009 |
Tang JW, Liebner TJ, Craven BA, Settles GS. A schlieren optical study of the human cough with and without wearing masks for aerosol infection control. Journal of the Royal Society, Interface / the Royal Society. 6: S727-36. PMID 19815575 DOI: 10.1098/Rsif.2009.0295.Focus |
0.321 |
|
2009 |
Craven BA, Paterson EG, Settles GS, Lawson MJ. Development and verification of a high-fidelity computational fluid dynamics model of canine nasal airflow. Journal of Biomechanical Engineering. 131: 091002. PMID 19725691 DOI: 10.1115/1.3148202 |
0.307 |
|
2009 |
Hargather MJ, Settles GS. Retroreflective shadowgraph technique for large-scale flow visualization. Applied Optics. 48: 4449-57. PMID 19649050 DOI: 10.1364/Ao.48.004449 |
0.335 |
|
2009 |
Hargather MJ, Settles GS. Laboratory-scale techniques for the measurement of a material response to an explosive blast International Journal of Impact Engineering. 36: 940-947. DOI: 10.1016/J.Ijimpeng.2008.12.008 |
0.333 |
|
2008 |
Biss MM, Settles GS, Staymates ME, Sanderson SR. Differential schlieren-interferometry with a simple adjustable Wollaston-like prism. Applied Optics. 47: 328-35. PMID 18204719 DOI: 10.1364/Ao.47.000328 |
0.742 |
|
2008 |
Kleine H, Settles GS. The art of shock waves and their flowfields Shock Waves. 17: 291-307. DOI: 10.1007/S00193-007-0118-6 |
0.324 |
|
2007 |
Staymates ME, Settles GS, Shi K, Liu Z. Supercontinuum laser illumination applied to traditional optical flow imaging methods Optics Communications. 273: 252-255. DOI: 10.1016/J.Optcom.2007.01.007 |
0.304 |
|
2007 |
Hargather MJ, Settles GS. Optical measurement and scaling of blasts from gram-range explosive charges Shock Waves. 17: 215-223. DOI: 10.1007/S00193-007-0108-8 |
0.352 |
|
2006 |
Settles GS. High-speed imaging of shock waves, explosions and gunshots American Scientist. 94: 22-31. DOI: 10.1511/2006.57.986 |
0.31 |
|
2006 |
Volpe JA, Settles GS. Laser-induced gas break-down as a light source for schlieren and shadow-graph particle image velocimetry Optical Engineering. 45. DOI: 10.1117/1.2332867 |
0.336 |
|
2006 |
Craven BA, Settles GS. A computational and experimental investigation of the human thermal plume Journal of Fluids Engineering, Transactions of the Asme. 128: 1251-1258. DOI: 10.1115/1.2353274 |
0.357 |
|
2006 |
Jonassen DR, Settles GS, Tronosky MD. Schlieren "pIV" for turbulent flows Optics and Lasers in Engineering. 44: 190-207. DOI: 10.1016/J.Optlaseng.2005.04.004 |
0.41 |
|
2005 |
Edge BA, Paterson EG, Settles GS. Computational study of the wake and contaminant transport of a walking human Journal of Fluids Engineering, Transactions of the Asme. 127: 967-977. DOI: 10.1115/1.2013291 |
0.368 |
|
2003 |
Pandya BH, Settles GS, Miller JD. Schlieren imaging of shock waves from a trumpet. The Journal of the Acoustical Society of America. 114: 3363-7. PMID 14714816 DOI: 10.1121/1.1628682 |
0.365 |
|
2003 |
Hartranft TJ, Settles GS. Sheet atomization of non-newtonian liquids Atomization and Sprays: Journal of the International Institutions For Liquid Atomization and Spray Systems. 13: 191-221. DOI: 10.1615/Atomizspr.V13.I23.30 |
0.721 |
|
2003 |
Settles GS, Keane BT, Anderson BW, Gatto JA. Shock waves in aviation security and safety Shock Waves. 12: 267-275. DOI: 10.1007/S00193-002-0162-1 |
0.362 |
|
2001 |
Gowadia HA, Settles GS. The natural sampling of airborne trace signals from explosives concealed upon the human body. Journal of Forensic Sciences. 46: 1324-31. PMID 11714142 DOI: 10.1520/Jfs15153J |
0.68 |
|
2001 |
Settles GS, McGann WJ. Potential for portal detection of human chemical and biological contamination Proceedings of Spie - the International Society For Optical Engineering. 4378: 1-9. DOI: 10.1117/12.438184 |
0.326 |
|
1998 |
Garg S, Settles GS. Measurements of a supersonic turbulent boundary layer by focusing schlieren deflectometry Experiments in Fluids. 25: 254-264. DOI: 10.1007/S003480050228 |
0.422 |
|
1997 |
Naughton JW, Cattafesta LN, Settles GS. An experimental study of compressible turbulent mixing enhancement in swirling jets Journal of Fluid Mechanics. 330: 271-305. DOI: 10.1017/S0022112096003679 |
0.361 |
|
1997 |
Lee Y, Garg S, Settles GS. Surface pressure measurements in shock wave/boundary-layer interactions Ksme International Journal. 11: 164-172. DOI: 10.1007/Bf02944890 |
0.41 |
|
1996 |
Garg S, Settles GS. Unsteady pressure loads generated by swept-shock-wave/boundary-layer interactions Aiaa Journal. 34: 1174-1181. DOI: 10.2514/3.13209 |
0.386 |
|
1996 |
Garrison TJ, Settles GS, Narayanswami N, Knight DD, Horstman CC. Flowfield surveys and computations of a crossing-shock wave/boundary-layer interaction Aiaa Journal. 34: 50-56. DOI: 10.2514/3.13020 |
0.443 |
|
1996 |
Garrison TJ, Settles GS, Horstman CC. Measurements of the triple shock wave/turbulent boundary-layer interaction Aiaa Journal. 34: 57-64. DOI: 10.2514/3.12864 |
0.461 |
|
1996 |
Scroggs SD, Settles GS. An experimental study of supersonic microjets Experiments in Fluids. 21: 401-409. DOI: 10.1007/Bf00189042 |
0.372 |
|
1995 |
Knight DD, Garrison TJ, Settles GS, Zheltovodov AA, Maksimov AI, Shevchenko AM, Vorontsov SS. Asymmetric crossing-shock-wave/turbulent-boundary-layer interaction Aiaa Journal. 33: 2241-2249. DOI: 10.2514/3.48361 |
0.437 |
|
1995 |
Knight DD, Garrison TJ, Settles GS, Zheltovodov AA, Maksimov AI, Shevchenko AM, Vorontsov SS. Asymmetric crossing shock wave - Turbulent boundary layer interaction 33rd Aerospace Sciences Meeting and Exhibit. |
0.305 |
|
1994 |
Settles GS, Dodson LJ. Supersonic and hypersonic shock/boundary-layer interaction database Aiaa Journal. 32: 1377-1383. DOI: 10.2514/3.12205 |
0.406 |
|
1994 |
Garrison TJ, Settles GS, Narayanswami N, Knight DD. Laser interferometer skin-friction measurements of crossing-shock-wave/turbulent-boundary-layer interactions Aiaa Journal. 32: 1234-1241. DOI: 10.2514/3.12125 |
0.411 |
|
1994 |
Lee Y, Settles GS, Horstman CC. Heat transfer measurements and computations of swept-shock-wave/boundary-layer interactions Aiaa Journal. 32: 726-734. DOI: 10.2514/3.12045 |
0.368 |
|
1993 |
Garrison TJ, Settles GS, Narayanswami N, Knight DD. Structure of crossing-shock-wave/turbulent-boundary-layer interactions Aiaa Journal. 31: 2204-2211. DOI: 10.2514/3.11916 |
0.412 |
|
1993 |
Naughton JW, Cattafesta LN, Settles GS. Miniature, fast-response five-hole conical probe for supersonic flowfield measurements Aiaa Journal. 31: 453-458. DOI: 10.2514/3.11351 |
0.344 |
|
1992 |
Knight DD, Badekas D, Horstman CC, Settles GS. Quasiconical Flowfield Structure of the Three-Dimensional Single Fin Interaction Aiaa Journal. 30: 2809-2816. DOI: 10.2514/3.48972 |
0.405 |
|
1992 |
Alvi FS, Settles GS. Physical model of the swept shock wave/boundary-layer interaction flowfield Aiaa Journal. 30: 2252-2258. DOI: 10.2514/3.11212 |
0.621 |
|
1991 |
Kim KS, Lee Y, Alvi FS, Settles GS, Horstman CC. Skin-friction measurements and computational comparison of swept shock/boundary-layer interactions Aiaa Journal. 29: 1643-1650. DOI: 10.2514/3.10786 |
0.665 |
|
1991 |
Kim KS, Lee Y, Settles GS. Laser interferometer/preston tube skin-friction comparison in shock/boundary-layer interaction Aiaa Journal. 29: 1007-1009. DOI: 10.2514/3.10695 |
0.445 |
|
1991 |
Lu FK, Settles GS. Inception length to a fully developed, fin-generated, shock-wave, boundary-layer interaction Aiaa Journal. 29: 758-762. DOI: 10.2514/3.10651 |
0.394 |
|
1990 |
Kim K, Settles GS. Skin friction measurements by laser interferometry in swept shock/boundary-layer interactions Aiaa Journal. 28: 133-139. DOI: 10.2514/3.10363 |
0.431 |
|
1990 |
Lu FK, Settles GS, Horstman CC. Mach number effects on conical surface features of swept shock-wave/boundary-layer interactions Aiaa Journal. 28: 91-97. DOI: 10.2514/3.10357 |
0.439 |
|
1990 |
Lu FK, Settles GS. Color surface-flow visualization of fin-generated shock wave boundary-layer interactions Experiments in Fluids. 8: 352-354. DOI: 10.1007/Bf00217200 |
0.39 |
|
1986 |
Settles GS, Horstman CC, McKenzie TM. EXPERIMENTAL AND COMPUTATIONAL STUDY OF A SWEPT COMPRESSION CORNER INTERACTION FLOWFIELD Aiaa Journal. 24: 744-752. DOI: 10.2514/3.9341 |
0.453 |
|
1986 |
Settles GS, Kimmel RL. Similarity of quasiconical shock wave/turbulent boundary-layer interactions Aiaa Journal. 24: 47-53. DOI: 10.2514/3.9221 |
0.45 |
|
1986 |
Settles GS, Lu FK. Reply by Authors to S.M. Bogdonoff and S. Wang Aiaa Journal. 24: 541-542. DOI: 10.2514/3.48663 |
0.443 |
|
1986 |
Schmidt MC, Settles GS. Alignment and application of the conical shadowgraph flow visualization technique Experiments in Fluids. 4: 93-96. DOI: 10.1007/Bf00266565 |
0.311 |
|
1985 |
Settles GS, Lu FK. Conical similarity of shock/boundary-layer interactions generated byswept and unswept fins Aiaa Journal. 23: 1021-1027. DOI: 10.2514/3.9033 |
0.45 |
|
1984 |
Settles GS, Teng H. Cylindrical and conical flow regimes of three-dimensional shock/boundary-layer interactions Aiaa Journal. 22: 194-200. DOI: 10.2514/3.8367 |
0.359 |
|
1983 |
Settles GS, Teng H. Flow visualization methods for separated three-dimensional shock wave/turbulent boundary-layer interactions Aiaa Journal. 21: 390-397. DOI: 10.2514/3.8085 |
0.415 |
|
1982 |
Settles GS, Bogdonoff SM. Scaling of Two- and Three-Dimensional Shock/Turbulent Boundary-Layer Interactions at Compression Corners Aiaa Journal. 20: 782-789. DOI: 10.2514/3.51135 |
0.724 |
|
1982 |
Horstman CC, Settles GS, Williams DR, Bogdonoff SM. REATTACHING FREE SHEAR LAYER IN COMPRESSIBLE TURBULENT FLOW Aiaa Journal. 20: 79-85. DOI: 10.2514/3.51049 |
0.748 |
|
1982 |
Settles GS, Williams DR, Baca BK, Bogdonoff SM. REATTACHMENT OF A COMPRESSIBLE TURBULENT FREE SHEAR LAYER Aiaa Journal. 20: 60-67. DOI: 10.2514/3.51047 |
0.746 |
|
1981 |
Horstman CC, Settles GS, Bogdonoff SM, Williams DR. REATTACHING FREE SHEAR LAYER IN COMPRESSIBLE TURBULENT FLOW - A COMPARISON OF NUMERICAL AND EXPERIMENTAL RESULTS Aiaa Paper. |
0.714 |
|
1980 |
Settles GS, Perkins JJ, Bogdonoff SM. Investigation of Three-Dimensional Shock/Boundary-Layer Interactions at Swept Compression Corners Aiaa Journal. 18: 779-785. DOI: 10.2514/3.50819 |
0.737 |
|
1980 |
Settles GS, Baca BK, Williams DR, Bogd SM. STUDY OF REATTACHMENT OF A FREE SHEAR LAYER IN COMPRESSIBLE TURBULENT FLOW Aiaa Paper. |
0.319 |
|
1979 |
Settles GS, Fitzpatrick TJ, Bogdonoff SM. Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow Aiaa Journal. 17: 579-585. DOI: 10.2514/3.61180 |
0.736 |
|
1977 |
Horstman CC, Settles GS, Vas IE, Bogdonoff SM, Hung CM. REYNOLDS NUMBER EFFECTS ON SHOCK-WAVE TURBULENT BOUNDARY-LAYER INTERACTIONS Aiaa Journal. 15: 1152-1158. DOI: 10.2514/3.60766 |
0.738 |
|
1976 |
Settles GS, Vas IE, Bogdonoff SM. Details of a Shock-Separated Turbulent Boundary Layer at a Compression Corner Aiaa Journal. 14: 1709-1715. DOI: 10.2514/3.61513 |
0.734 |
|
1976 |
Settles GS, Bogdonoff SM, Vas IE. Incipient Separation of a Supersonic Turbulent Boundary Layer at High Reynolds Numbers Aiaa Journal. 14: 50-56. DOI: 10.2514/3.61331 |
0.731 |
|
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