Year |
Citation |
Score |
2014 |
Todd Lowe K, Byun G, Simpson RL. The effect of particle lag on supersonic turbulent boundary layer statistics 52nd Aerospace Sciences Meeting. |
0.384 |
|
2014 |
Todd Lowe K, Byun G, Simpson RL. The effect of particle lag on supersonic turbulent boundary layer statistics 52nd Aerospace Sciences Meeting. |
0.384 |
|
2013 |
Lowe KT, Maisto P, Byun G, Simpson RL, Verkamp M, Danehy PM, Tiemsin PI, Wohl CJ. Laser velocimetry with fluorescent dye-doped polystyrene microspheres. Optics Letters. 38: 1197-9. PMID 23595429 DOI: 10.1364/Ol.38.001197 |
0.698 |
|
2013 |
Lowe KT, Byun G, Neuhart DH, Simpson RL. Auto-calibration of spatially-resolving laser-Doppler velocimeters 51st Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013. |
0.331 |
|
2012 |
Lowe KT, Simpson RL, Neale TP. A laser-Doppler velocimeter system for near-field velocity vector measurements in large facilities 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.2514/6.2012-693 |
0.404 |
|
2012 |
Rusche MT, Simpson RL. Structure of turbulent boundary layers and surface pressure fluctuations on a patch of roughness elements 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.2514/6.2012-1107 |
0.419 |
|
2010 |
Byun G, Simpson RL. Surface-pressure fluctuations from separated flow over an axisymmetric bump Aiaa Journal. 48: 2397-2405. DOI: 10.2514/1.J050429 |
0.728 |
|
2010 |
Sadek SA, Simpson RL. A basic three-dimensional turbulent boundary layer experiment to test second-moment closure models 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.467 |
|
2010 |
Hopkins AMR, Simpson RL. Structure of turbulent boundary layers with dense roughness 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.421 |
|
2010 |
Byun G, Simpson RL. Characteristics of separated flow surface pressure fluctuations on an axisymmetric bump 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.417 |
|
2010 |
Varano ND, Simpson RL. Structure of turbulent boundary layers and surface pressure fluctuations with sparse roughness 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.453 |
|
2010 |
DeMoss JA, Simpson RL. Measurements of the steady skin friction and cross-flow separation location on an ellipsoidal model in yaw or pitch over a range of roll angles 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.367 |
|
2009 |
Lowe KT, Simpson RL. An advanced laser-Doppler velocimeter for full-vector particle position and velocity measurements Measurement Science and Technology. 20. DOI: 10.1088/0957-0233/20/4/045402 |
0.413 |
|
2009 |
Hopkins AMR, Simpson RL. Fluid dynamics and surface pressure fluctuations of dense rough surface turbulent boundary layers 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.365 |
|
2009 |
DeMoss JA, Simpson RL. A study of the boundary layer development, skin friction, and wake on a non-body of revolution ellipsoidal model 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.429 |
|
2009 |
Varano ND, Simpson RL. Flow structure and pressure fluctuations of turbulent boundary layers with sparse roughness 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.505 |
|
2008 |
Todd Lowe K, Simpson RL. Turbulence structural measurements using a comprehensive laser-Doppler velocimeter in two- and three-dimensional turbulent boundary layers International Journal of Heat and Fluid Flow. 29: 820-829. DOI: 10.1016/j.ijheatfluidflow.2008.03.003 |
0.481 |
|
2008 |
Ölçmen SM, Simpson RL. Experimental transport-rate budgets in complex 3-D turbulent flow near a wing/body junction International Journal of Heat and Fluid Flow. 29: 874-890. DOI: 10.1016/J.Ijheatfluidflow.2007.12.004 |
0.541 |
|
2007 |
Hosder S, Simpson RL. Experimental investigation of unsteady flow separation on a maneuvering axisymmetric body Journal of Aircraft. 44: 1286-1295. DOI: 10.2514/1.26804 |
0.477 |
|
2007 |
Ölcmen S, Simpson RL. Influence of passive flow-control devices on the pressure fluctuations at wing-body junction flows Journal of Fluids Engineering, Transactions of the Asme. 129: 1030-1037. DOI: 10.1115/1.2746917 |
0.46 |
|
2007 |
Tian Q, Lowe KT, Simpson RL. A three-velocity-component laser-Doppler velocimeter for measurements inside the linear compressor cascade Experiments in Fluids. 43: 487-499. DOI: 10.1007/S00348-007-0311-5 |
0.619 |
|
2007 |
Tian Q, Simpson RL. Experimental study of tip leakage flow in the linear compressor cascade: Part II - Effect of moving wall Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 5: 3345-3362. |
0.48 |
|
2007 |
Tian Q, Simpson RL. Experimental study of tip leakage flow in the linear compressor cascade: Part 1 - Stationary wall Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 5: 3321-3344. |
0.479 |
|
2006 |
Tang G, Simpson RL, Tian Q. Experimental study of tip-gap turbulent flow structure Proceedings of the Asme Turbo Expo. 6: 175-183. DOI: 10.1115/GT2006-90359 |
0.5 |
|
2006 |
Ölçmen SM, Simpson RL, Newby JW. Octant analysis based structural relations for three-dimensional turbulent boundary layers Physics of Fluids. 18. DOI: 10.1063/1.2172650 |
0.498 |
|
2006 |
Ölçmen SM, Simpson RL. Some features of a turbulent wing-body junction vortical flow International Journal of Heat and Fluid Flow. 27: 980-993. DOI: 10.1016/J.Ijheatfluidflow.2006.02.019 |
0.6 |
|
2006 |
Lowe KT, Simpson RL. Measurements of velocity-acceleration statistics in turbulent boundary layers International Journal of Heat and Fluid Flow. 27: 558-565. DOI: 10.1016/j.ijheatfluidflow.2006.02.003 |
0.456 |
|
2006 |
George J, Simpson RL. Propagation of vorticity and turbulence in 2-D and 3-D rough-wall turbulent boundary layers Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 6: 3862-3907. |
0.394 |
|
2005 |
Byun G, Simpson RL. Structure of three-dimensional separated flow on an axisymmetric bump 43rd Aiaa Aerospace Sciences Meeting and Exhibit - Meeting Papers. 10235-10248. DOI: 10.2514/1.17002 |
0.772 |
|
2005 |
Simpson RL. Some observations on the structure and modeling of 3-D turbulent boundary layers and separated flow 4th International Symposium On Turbulence and Shear Flow Phenomena. 1: 1-10. |
0.507 |
|
2005 |
Ma R, Simpson RL. Characterization of turbulent flow downstream of a three-dimensional axisymmetric bump 4th International Symposium On Turbulence and Shear Flow Phenomena. 3: 1171-1176. |
0.509 |
|
2004 |
Byun G, Simpson RL, Long CH. Study of Vortical Separation from Three-Dimensional Symmetric Bumps Aiaa Journal. 42: 754-765. DOI: 10.2514/1.1829 |
0.772 |
|
2004 |
Tian Q, Simpson RL, Tang G. Flow visualization on the linear compressor cascade endwall using oil flows and laser Doppler anemometry Measurement Science and Technology. 15: 1910-1916. DOI: 10.1088/0957-0233/15/9/031 |
0.694 |
|
2004 |
Byun G, Ölçmen SM, Simpson RL. A miniature laser-Doppler velocimeter for simultaneous three-velocity-component measurements Measurement Science and Technology. 15: 2075-2082. DOI: 10.1088/0957-0233/15/10/018 |
0.739 |
|
2004 |
George J, Simpson RL. Transport-rate budgets of Reynolds stresses in 2-D and 3-D rough-wall turbulent boundary layers Aiaa Paper. 10083-10102. |
0.311 |
|
2003 |
George J, Simpson RL. Roughness effects on turbulent boundary layers - contributions to a conceptual model 41st Aerospace Sciences Meeting and Exhibit. |
0.312 |
|
2003 |
Byun G, Simpson RL, Long CH. A study of vortical separation from three-dimensional symmetric bumps 41st Aerospace Sciences Meeting and Exhibit. |
0.514 |
|
2002 |
Simpson RL, Long CH, Byun G. Study of vortical separation from an axisymmetric hill International Journal of Heat and Fluid Flow. 23: 582-591. DOI: 10.1016/S0142-727X(02)00154-6 |
0.773 |
|
2002 |
Simpson RL. Some Reynolds number effects on separating 2-D and attached 3-D turbulent boundary layers 40th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.505 |
|
2002 |
George J, Simpson RL. Some three-dimensional rough-wall turbulent boundary layers 40th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.462 |
|
2001 |
Ölçmen MS, Simpson RL, Goody M. An Experimental Investigation of Two-Point Correlations in Two- and Three-Dimensional Turbulent Boundary Layers Flow, Turbulence and Combustion. 66: 85-112. DOI: 10.1023/A:1017576627047 |
0.486 |
|
2001 |
Ölçmen MS, Simpson RL, George J. Some Reynolds number effects on two- and three-dimensional turbulent boundary layers Experiments in Fluids. 31: 219-228. DOI: 10.1007/S003480100276 |
0.588 |
|
2001 |
Simpson RL. Junction flows Annual Review of Fluid Mechanics. 33: 415-443. |
0.48 |
|
2001 |
Hosder S, Simpson RL. Unsteady turbulent skin friction and separation location measurements on a maneuvering undersea vehicle 39th Aerospace Sciences Meeting and Exhibit. |
0.349 |
|
2000 |
Goody MC, Simpson RL, Chesnakas CJ. Separated Flow Surface Pressure Fluctuations and Pressure-Velocity Correlations on Prolate Spheroid Aiaa Journal. 38: 266-274. DOI: 10.2514/2.953 |
0.531 |
|
2000 |
Goody MC, Simpson RL. Surface Pressure Fluctuations Beneath Two- and Three-Dimensional Turbulent Boundary Layers Aiaa Journal. 38: 1822-1831. DOI: 10.2514/2.863 |
0.522 |
|
1998 |
Lewis DJ, Simpson RL. a Three-Dimensional Turbulent Boundary Layer Turbulence Structure of Heat Transfer Through Journal of Thermophysics and Heat Transfer. 12: 248-255. DOI: 10.2514/2.6328 |
0.418 |
|
1998 |
Neel RE, Walters RW, Simpson RL. Computations of Steady and Unsteady Low-Speed Turbulent Separated Flows Aiaa Journal. 36: 1208-1215. DOI: 10.2514/2.501 |
0.51 |
|
1998 |
Wetzel TG, Simpson RL, Chesnakas CJ. Measurement of Three-Dimensional Crossflow Separation Aiaa Journal. 36: 557-564. DOI: 10.2514/2.429 |
0.442 |
|
1998 |
Wetzel TG, Simpson RL. Unsteady Crossflow Separation Location Measurements on a Maneuvering 6:1 Prolate Spheroid Aiaa Journal. 36: 2063-2071. DOI: 10.2514/2.307 |
0.378 |
|
1998 |
Wetzel TG, Simpson RL. Effects of fin and jet vortex generators on the crossflow Journal of Aircraft. 35: 370-379. DOI: 10.2514/2.2334 |
0.46 |
|
1997 |
Chesnakas CJ, Taylor D, Simpson RL. Detailed Investigation of the Three-Dimensional Separation About a 6:1 Prolate Spheroid Aiaa Journal. 35: 990-999. DOI: 10.2514/2.208 |
0.513 |
|
1997 |
Hytopoulos E, Schetz JA, Simpson RL. Turbulence Model for Steady and Unsteady Boundary Layers in Strong Pressure Gradients Journal of Fluids Engineering. 119: 541-549. DOI: 10.1115/1.2819278 |
0.521 |
|
1996 |
Chesnakas CJ, Simpson RL. Measurements of the Turbulence Structure in the Vicinity of a 3-D Separation Journal of Fluids Engineering. 118: 268-275. DOI: 10.1115/1.2817373 |
0.44 |
|
1996 |
O¨lc¸men MS, Simpson RL. An Experimental Study of a Three-Dimensional Pressure-Driven Turbulent Boundary Layer Journal of Fluids Engineering. 118: 416-418. DOI: 10.1017/S0022112095002497 |
0.597 |
|
1996 |
Simpson RL. Aspects of turbulent boundary-layer separation Progress in Aerospace Sciences. 32: 457-521. DOI: 10.1016/0376-0421(95)00012-7 |
0.575 |
|
1995 |
Ozcan O, Johnson DA, Simpson RL. Comment on 'Wakes of three axisymmetric bodies at zero angle of attack' Aiaa Journal. 33: 569-570. DOI: 10.2514/3.12410 |
0.438 |
|
1995 |
Olcmen SM, Simpson RL. A five-velocity-component laser-Doppler velocimeter for measurements of a three-dimensional turbulent boundary layer Measurement Science and Technology. 6: 702-716. DOI: 10.1088/0957-0233/6/6/009 |
0.537 |
|
1994 |
Lewis DJ, Simpson RL, Diller TE. Time-resolved surface heat flux measurements in the wing/body junction vortex Journal of Thermophysics and Heat Transfer. 8: 656-663. DOI: 10.2514/3.595 |
0.339 |
|
1994 |
Olcmen SM, Simpson RL. Influence of Wing Shapes on Surface Pressure Fluctuations at Wing-Body Junctions Aiaa Journal. 32: 6-15. DOI: 10.2514/3.48283 |
0.446 |
|
1993 |
Olcmen MS, Simpson RL. Evaluation of algebraic eddy-viscosity models in three-dimensional turbulent boundary-layer flows Aiaa Journal. 31: 1545-1554. DOI: 10.2514/3.11813 |
0.487 |
|
1993 |
Fleming JL, Simpson RL, Cowling JE, Devenport WJ. An experimental study of a turbulent wing-body junction and wake flow Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow. 14: 366-378. DOI: 10.1007/Bf00189496 |
0.568 |
|
1992 |
Agarwal NK, Simpson RL, Shivaprasad BG. Some effects of oscillation waveform and amplitude on unsteady turbulent shear flows Journal of Propulsion and Power. 8: 674-679. DOI: 10.2514/3.23531 |
0.562 |
|
1992 |
Devenport WJ, Simpson RL, Dewitz MB, Agarwal NK. Effects of a leading-edge fillet on the flow past an appendage-body junction Aiaa Journal. 30: 2177-2183. DOI: 10.2514/3.11201 |
0.552 |
|
1992 |
Devenport WJ, Simpson RL. Flow past a wing-body junction - Experimental evaluation of turbulence models Aiaa Journal. 30: 873-881. DOI: 10.2514/3.11004 |
0.549 |
|
1992 |
O¨lc¸men MS, Simpson RL. Perspective: On the Near Wall Similarity of Three-Dimensional Turbulent Boundary Layers (Data Bank Contribution) Journal of Fluids Engineering. 114: 487-495. DOI: 10.1115/1.2910059 |
0.563 |
|
1991 |
Simpson RL. The structure of the near-wall region of two-dimensional turbulent separated flow Philosophical Transactions of the Royal Society A. 336: 5-17. DOI: 10.1098/Rsta.1991.0063 |
0.552 |
|
1990 |
Devenport WJ, Agarwal NK, Dewitz MB, Simpson RL, Poddar K. Effects of a Fillet on the Flow Past a Wing-Body Junction Aiaa Journal. 28: 2017-2024. DOI: 10.2514/3.10517 |
0.527 |
|
1990 |
Agarwal NK, Simpson RL. Backflow Structure Of Steady And Unsteady Separating Turbulent Boundary Layers Aiaa Journal. 28: 1764-1771. DOI: 10.2514/3.10472 |
0.548 |
|
1990 |
Simpson RL, Agarwal NK, Nagabushana KA, Olcmen S. Spectral measurements and other features of separating turbulent flows Aiaa Journal. 28: 446-452. DOI: 10.2514/3.10413 |
0.567 |
|
1990 |
Devenport WJ, Simpson RL. Time-dependent and time-averaged turbulence structure near the nose of a wing-body junction Journal of Fluid Mechanics. 210: 23-55. DOI: 10.1017/S0022112090001215 |
0.609 |
|
1988 |
Simpson R. Book Review: Advances in Turbulence (Proceedings of the First European Turbulence Conference, Lyon, France, duly 1 -4, 1986), Comte-Bellot and J. Mathieu, Editors Aiaa Journal. 26: 508-508. DOI: 10.2514/3.48771 |
0.391 |
|
1988 |
Chew YT, Simpson RL. An Explicit Non-Real Time Data Reduction Method of Triple Sensors Hot-Wire Anemometer in Three-Dimensional Flow Journal of Fluids Engineering-Transactions of the Asme. 110: 110-119. DOI: 10.1115/1.3243521 |
0.36 |
|
1987 |
Simpson RL. Two-dimensional turbulent separated flow Aiaa Journal. 25: 775-776. DOI: 10.2514/3.9699 |
0.539 |
|
1985 |
Saripalli KR, Simpson RL. Measurements of a zero-pressure-gradient boundary layer blown by an asymmetric jet Aiaa Journal. 23: 490-491. DOI: 10.2514/3.8941 |
0.344 |
|
1981 |
Simpson RL. Review—A Review of Some Phenomena in Turbulent Flow Separation Journal of Fluids Engineering. 103: 520-533. DOI: 10.1115/1.3241761 |
0.389 |
|
1978 |
Simpson RL, Sallas JJ, Nasburg RE. Tailoring the Waveform of a Periodic Flow With a Programmable Damper Journal of Fluids Engineering. 100: 287-290. DOI: 10.1115/1.3448668 |
0.39 |
|
1973 |
SIMPSON RL. A generalized correlation of roughness density effects on the turbulent boundary layer. Aiaa Journal. 11: 242-244. DOI: 10.2514/3.6736 |
0.303 |
|
1971 |
Simpson RL. The effect of a discontinuity in wall blowing on the turbulent incompressible boundary layer International Journal of Heat and Mass Transfer. 14: 2083-2097. DOI: 10.1016/0017-9310(71)90029-9 |
0.457 |
|
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