| Year |
Citation |
Score |
| 2020 |
Joseph LA, Molinaro NJ, Devenport WJ, Meyers TW. Characteristics of the pressure fluctuations generated in turbulent boundary layers over rough surfaces Journal of Fluid Mechanics. 883. DOI: 10.1017/Jfm.2019.813 |
0.495 |
|
| 2020 |
Awasthi M, Devenport WJ, Glegg SAL. Sound radiated by turbulent flow over unrounded and rounded forward-facing steps Journal of Sound and Vibration. 488: 115635. DOI: 10.1016/J.Jsv.2020.115635 |
0.515 |
|
| 2019 |
Awasthi M, Devenport WJ, Alexander WN, Glegg SAL. Aeroacoustics of Rounded Forward-Facing Steps: Far-Field Behavior Aiaa Journal. 57: 1237-1249. DOI: 10.2514/1.J057086 |
0.381 |
|
| 2019 |
Brown K, Devenport W, Borgoltz A. Exploitation of hybrid anechoic wind tunnels for aeroacoustic and aerodynamic measurements Ceas Aeronautical Journal. 10: 251-266. DOI: 10.1007/S13272-019-00385-2 |
0.807 |
|
| 2018 |
Brown K, Molinaro N, Meyers T, Borgoltz A, Devenport W, Luedke J, Pesetsky D. Sensitivity of wind turbine airfoil sections to geometry variations inherent in modular blades Wind Engineering. 42: 529-546. DOI: 10.1177/0309524X18780376 |
0.816 |
|
| 2018 |
Devenport W, Alexander N, Glegg S, Wang M. The Sound of Flow Over Rigid Walls Annual Review of Fluid Mechanics. 50: 435-458. DOI: 10.1146/Annurev-Fluid-122316-045056 |
0.539 |
|
| 2018 |
Murray HH, Devenport WJ, Alexander WN, Glegg SAL, Wisda D. Aeroacoustics of a rotor ingesting a planar boundary layer at high thrust Journal of Fluid Mechanics. 850: 212-245. DOI: 10.1017/Jfm.2018.438 |
0.491 |
|
| 2018 |
Brown K, Brown J, Patil M, Devenport W. Inverse measurement of wall pressure field in flexible-wall wind tunnels using global wall deformation data Experiments in Fluids. 59: 25. DOI: 10.1007/S00348-017-2477-9 |
0.499 |
|
| 2017 |
Alexander WN, Devenport WJ, Glegg SAL. Noise from a rotor ingesting a thick boundary layer and relation to measurements of ingested turbulence Journal of Sound and Vibration. 409: 227-240. DOI: 10.1016/J.Jsv.2017.07.056 |
0.542 |
|
| 2016 |
Moreau DJ, Doolan CJ, Nathan Alexander W, Meyers TW, Devenport WJ. Wall-mounted finite airfoil-noise production and prediction Aiaa Journal. 54: 1637-1651. DOI: 10.2514/1.J054493 |
0.423 |
|
| 2016 |
Clark IA, Daly CA, Devenport W, Alexander WN, Peake N, Jaworski JW, Glegg S. Bio-inspired canopies for the reduction of roughness noise Journal of Sound and Vibration. 385: 33-54. DOI: 10.1016/J.Jsv.2016.08.027 |
0.469 |
|
| 2016 |
Joseph LA, Borgoltz A, Devenport W. Infrared thermography for detection of laminar-turbulent transition in low—speed wind tunnel testing Experiments in Fluids. 57. DOI: 10.1007/S00348-016-2162-4 |
0.805 |
|
| 2016 |
Joseph LA, Meyers TW, Molinaro NJ, Devenport WJ, Glegg S. Pressure fluctuations in a high-reynolds-number turbulent boundary layer over rough surfaces of different element spacing 22nd Aiaa/Ceas Aeroacoustics Conference, 2016. |
0.395 |
|
| 2015 |
Kuester MS, Brown K, Meyers T, Intaratep N, Borgoltz A, Devenport WJ. Wind tunnel testing of airfoils for wind turbine applications Wind Engineering. 39: 651-660. DOI: 10.1260/0309-524X.39.6.651 |
0.802 |
|
| 2015 |
Meyers T, Forest JB, Devenport WJ. The wall-pressure spectrum of high-Reynolds-number turbulent boundary-layer flows over rough surfaces Journal of Fluid Mechanics. 768: 261-293. DOI: 10.1017/Jfm.2014.743 |
0.49 |
|
| 2015 |
Glegg SAL, Devenport W, Alexander N. Broadband rotor noise predictions using a time domain approach Journal of Sound and Vibration. 335: 115-124. DOI: 10.1016/J.Jsv.2014.09.007 |
0.536 |
|
| 2015 |
Moreau DJ, Doolan CJ, Nathan Alexander W, Meyers TW, Devenport WJ. Wall-mounted finite airfoil noise production and prediction 21st Aiaa/Ceas Aeroacoustics Conference. |
0.425 |
|
| 2014 |
Alexander WN, Devenport WJ, Glegg SAL. Predictive limits of acoustic diffraction theory for rough wall flows Aiaa Journal. 52: 634-642. DOI: 10.2514/1.J052561 |
0.545 |
|
| 2014 |
Awasthi M, Devenport WJ, Glegg SAL, Forest JB. Pressure fluctuations produced by forward steps immersed in a turbulent boundary layer Journal of Fluid Mechanics. 756: 384-421. DOI: 10.1017/Jfm.2014.405 |
0.437 |
|
| 2014 |
Catlett MR, Devenport W, Glegg SAL. Sound from boundary layer flow over steps and gaps Journal of Sound and Vibration. 333: 4170-4186. DOI: 10.1016/J.Jsv.2014.03.042 |
0.457 |
|
| 2014 |
Moreau DJ, Doolan CJ, Alexander WN, Meyers TW, Devenport WJ. Experimental investigation of wall-mounted finite airfoil flow noise Proceedings of the 19th Australasian Fluid Mechanics Conference, Afmc 2014. |
0.432 |
|
| 2013 |
Alexander WN, Devenport WJ, Glegg SAL. Predictions of sound from rough wall boundary layers Aiaa Journal. 51: 465-475. DOI: 10.2514/1.J051840 |
0.514 |
|
| 2013 |
Devenport WJ, Burdisso RA, Borgoltz A, Ravetta PA, Barone MF, Brown KA, Morton MA. The Kevlar-walled anechoic wind tunnel Journal of Sound and Vibration. 332: 3971-3991. DOI: 10.1016/J.Jsv.2013.02.043 |
0.827 |
|
| 2013 |
Awasthi M, Bryan B, Devenport WJ, Glegg SAL. Sound radiation from rounded steps and gaps 19th Aiaa/Ceas Aeroacoustics Conference. 47. |
0.321 |
|
| 2011 |
Devenport WJ, Grissom DL, Nathan Alexander W, Smith BS, Glegg SAL. Measurements of roughness noise Journal of Sound and Vibration. 330: 4250-4273. DOI: 10.1016/J.Jsv.2011.03.017 |
0.83 |
|
| 2011 |
Larssen JV, Devenport WJ. On the generation of large-scale homogeneous turbulence Experiments in Fluids. 50: 1207-1223. DOI: 10.1007/S00348-010-0974-1 |
0.834 |
|
| 2010 |
Glegg S, Devenport W. The noise from flow over rough surfaces with small and large roughness elements. Journal of the Acoustical Society of America. 127: 1796-1796. DOI: 10.1121/1.3384028 |
0.501 |
|
| 2010 |
Devenport W, Wahl EA, Glegg SAL, Alexander WN, Grissom DL. Measuring surface pressure with far field acoustics Journal of Sound and Vibration. 329: 3958-3971. DOI: 10.1016/J.Jsv.2010.03.012 |
0.83 |
|
| 2010 |
Glegg SAL, Devenport WJ. Panel methods for airfoils in turbulent flow Journal of Sound and Vibration. 329: 3709-3720. DOI: 10.1016/J.Jsv.2010.03.007 |
0.526 |
|
| 2010 |
Devenport WJ, Staubs JK, Glegg SAL. Sound radiation from real airfoils in turbulence Journal of Sound and Vibration. 329: 3470-3483. DOI: 10.1016/J.Jsv.2010.02.022 |
0.824 |
|
| 2010 |
Devenport WJ, Burdisso RA, Borgoltz A, Ravetta P, Barone MF. Aerodynamic and acoustic corrections for a Kevlar-walled anechoic wind tunnel 16th Aiaa/Ceas Aeroacoustics Conference (31st Aiaa Aeroacoustics Conference). |
0.806 |
|
| 2009 |
Glegg SAL, Devenport WJ, Spitz N. Application of proper orthogonal decomposition to trailing-edge noise Aiaa Journal. 47: 1543-1548. DOI: 10.2514/1.41921 |
0.417 |
|
| 2009 |
Glegg S, Devenport W. The far-field sound from rough-wall boundary layers Proceedings of the Royal Society a: Mathematical, Physical and Engineering Sciences. 465: 1717-1734. DOI: 10.1098/Rspa.2008.0318 |
0.441 |
|
| 2009 |
Glegg SAL, Devenport W. Unsteady loading on an airfoil of arbitrary thickness Journal of Sound and Vibration. 319: 1252-1270. DOI: 10.1016/J.Jsv.2008.06.053 |
0.493 |
|
| 2008 |
Ma R, Devenport WJ. Unsteady aperiodic behavior of a periodically disturbed tip-leakage vortex Aiaa Journal. 46: 1025-1038. DOI: 10.2514/1.13539 |
0.642 |
|
| 2008 |
Blake W, Kim KH, Goody M, Wang M, Devenport WJ, Glegg SAL. Investigations of roughness-generated TBL sound using coupled physical-computational experiments in conjunction with theoretical development Proceedings - European Conference On Noise Control. 1059-1064. DOI: 10.1121/1.2933067 |
0.47 |
|
| 2008 |
Devenport WJ, Glegg SA, Alexander N, Smith B. The mechanisms of roughness noise Journal of the Acoustical Society of America. 123: 3023-3023. DOI: 10.1121/1.2932648 |
0.54 |
|
| 2008 |
Remillieux MC, Burdisso RA, Devenport WJ. Preliminary screening of flow behavior around airfoils using a microphone phased array The Journal of the Acoustical Society of America. 123: 3022-3022. DOI: 10.1121/1.2932643 |
0.561 |
|
| 2008 |
Staubs JK, Devenport WJ, Glegg SAL. Sound radiation from a series of airfoils immersed in grid- generated turbulence 14th Aiaa/Ceas Aeroacoustics Conference (29th Aiaa Aeroacoustics Conference). |
0.814 |
|
| 2008 |
Remillieux MC, Crede ED, Camargo HE, Burdisso RA, Devenport WJ, Rasnick M, Van Seeters P, Chou A. Calibration and demonstration of the new Virginia Tech anechoic wind tunnel 14th Aiaa/Ceas Aeroacoustics Conference (29th Aiaa Aeroacoustics Conference). |
0.391 |
|
| 2007 |
Ma R, Devenport WJ. Tip gap effects on the unsteady behavior of a tip leakage vortex Aiaa Journal. 45: 1713-1724. DOI: 10.2514/1.13536 |
0.681 |
|
| 2007 |
Grissom DL, Smith B, Devenport WJ, Glegg SAL. Rough-wall boundary layer noise: An experimental investigation 13th Aiaa/Ceas Aeroacoustics Conference (28th Aiaa Aeroacoustics Conference). |
0.843 |
|
| 2006 |
Ma R, Devenport WJ. Unsteady periodic behavior of a disturbed tip-leakage flow Aiaa Journal. 44: 1073-1086. DOI: 10.2514/1.12082 |
0.695 |
|
| 2006 |
Mish PF, Devenport WJ. An experimental investigation of unsteady surface pressure on an airfoil in turbulence-Part 2: Sources and prediction of mean loading effects Journal of Sound and Vibration. 296: 447-460. DOI: 10.1016/J.Jsv.2005.08.009 |
0.835 |
|
| 2006 |
Mish PF, Devenport WJ. An experimental investigation of unsteady surface pressure on an airfoil in turbulence-Part 1: Effects of mean loading Journal of Sound and Vibration. 296: 417-446. DOI: 10.1016/J.Jsv.2005.08.008 |
0.817 |
|
| 2006 |
Borgoltz A, Devenport WJ, Craig L. Space-time correlations and trailing edge flow structure in fan-blade wakes with trailing edge blowing Collection of Technical Papers - 12th Aiaa/Ceas Aeroacoustics Conference. 2: 1026-1054. |
0.828 |
|
| 2006 |
Glegg S, Devenport WJ, Staubs JK. Leading edge noise Collection of Technical Papers - 12th Aiaa/Ceas Aeroacoustics Conference. 1: 310-340. |
0.832 |
|
| 2006 |
Grissom DL, Smith B, Devenport WJ, Glegg SAL. Rough-wall boundary layer noise Collection of Technical Papers - 12th Aiaa/Ceas Aeroacoustics Conference. 1: 121-136. |
0.82 |
|
| 2005 |
Borgoltz A, Elizabeth Craig M, Devenport WJ. Trailing edge blowing of fan blades Collection of Technical Papers - 11th Aiaa/Ceas Aeroacoustics Conference. 4: 2855-2875. |
0.83 |
|
| 2005 |
Grissom DL, Devenport WJ, Glegg SAL. Measurements of a discrete upwash gust passing through a linear flat plate cascade, and comparisons with linearized theory Collection of Technical Papers - 11th Aiaa/Ceas Aeroacoustics Conference. 3: 1991-2013. |
0.795 |
|
| 2005 |
Smith BS, Camargo HE, Burdisso RA, Devenport WJ. Development and testing of a novel acoustic wind tunnel concept Collection of Technical Papers - 11th Aiaa/Ceas Aeroacoustics Conference. 5: 3153-3173. |
0.417 |
|
| 2004 |
Wenger CW, Devenport WJ, Wittmer KS, Muthanna C. Wake of a compressor cascade with tip gap, part 3: Two-point statistics Aiaa Journal. 42: 2341-2346. DOI: 10.2514/1.842 |
0.529 |
|
| 2004 |
Wang Y, Devenport WJ. Wake of a compressor cascade with tip gap, part 2: Effects of endwall motion Aiaa Journal. 42: 2332-2340. DOI: 10.2514/1.5272 |
0.439 |
|
| 2004 |
Muthanna C, Devenport WJ. Wake of a compressor cascade with tip gap, part 1: Mean flow and turbulence structure Aiaa Journal. 42: 2320-2331. DOI: 10.2514/1.5270 |
0.524 |
|
| 2004 |
De La Riva DH, Devenport WJ, Muthanna C, Glegg SAL. Behavior of turbulence flowing through a compressor cascade Aiaa Journal. 42: 1302-1313. DOI: 10.2514/1.3107 |
0.539 |
|
| 2004 |
Staubs J, Mish P, Devenport WJ. Correlation between unsteady loading and tip gap flow occurring in a linear cascade produced by simulated stator-rotor interaction Proceedings of the Asme Heat Transfer/Fluids Engineering Summer Conference 2004, Ht/Fed 2004. 3: 313-331. DOI: 10.1115/Ht-Fed2004-56853 |
0.785 |
|
| 2004 |
Grissom DL, Devenport WJ. Development and testing of a deterministic disturbance generator Collection of Technical Papers - 10th Aiaa/Ceas Aeroacoustics Conference. 2: 1765-1779. |
0.82 |
|
| 2004 |
Intaratep N, Devenport WJ, Staubs J. The tip leakage vortex shed from an unsteady tip clearance flow 34th Aiaa Fluid Dynamics Conference and Exhibit. |
0.839 |
|
| 2004 |
Borgoltz A, Geiger D, Devenport WJ. Analysis of wakes shed by idealized aircraft engine fan blades for noise reduction Collection of Technical Papers - 10th Aiaa/Ceas Aeroacoustics Conference. 2: 1257-1288. |
0.827 |
|
| 2004 |
Glegg SAL, Devenport WJ, Spitz N. The application of proper orthogonal decomposition to trailing edge noise Collection of Technical Papers - 10th Aiaa/Ceas Aeroacoustics Conference. 2: 1245-1256. |
0.4 |
|
| 2003 |
Larssen JV, Devenport WJ. Interaction of large scale homogeneous turbulence with a cascade of flat plates 41st Aerospace Sciences Meeting and Exhibit. |
0.794 |
|
| 2003 |
Boquilion O, Glegg S, Larssen JV, Devenport WJ. The interaction of large scale turbulence with a cascade of flat plates 9th Aiaa/Ceas Aeroacoustics Conference and Exhibit. |
0.838 |
|
| 2003 |
Casper J, Farassat F, Mish PF, Devenport WJ. Broadband noise predictions for an airfoil in a turbulent stream 41st Aerospace Sciences Meeting and Exhibit. |
0.816 |
|
| 2003 |
Spitz N, Devenport WJ, Glegg SAL. Predicting modes of the unsteady vorticity field near the trailing edge of a blade 9th Aiaa/Ceas Aeroacoustics Conference and Exhibit. |
0.31 |
|
| 2002 |
Larssen JV, Devenport WJ. The generation of high reynolds number homogeneous turbulence 32nd Aiaa Fluid Dynamics Conference and Exhibit. |
0.838 |
|
| 2002 |
Mish PF, Devenport WJ, Borgoltz AG. Evaluation and further analysis of unsteady pressure response measurements on an airfoil at angle of attack 8th Aiaa/Ceas Aeroacoustics Conference and Exhibit. |
0.792 |
|
| 2001 |
Devenport WJ, Muthanna C, Ma R, Glegg SAL. Two-point descriptions of wake turbulence with application to noise prediction Aiaa Journal. 39: 2302-2307. DOI: 10.2514/2.1235 |
0.64 |
|
| 2001 |
Glegg SAL, Devenport WJ. Proper orthogonal decomposition of turbulent flows for aeroacoustic and hydroacoustic applications Journal of Sound and Vibration. 239: 767-784. DOI: 10.1006/Jsvi.2000.3128 |
0.499 |
|
| 2001 |
Mistf PF, Devenport WJ. Mean loading effects on the surface pressure fluctuations on an airfoil in turbulence 7th Aiaa/Ceas Aeroacoustics Conference and Exhibit. |
0.412 |
|
| 2001 |
Glegg SAL, Devenport WJ. Rotor/stator interaction noise from blade wakes 7th Aiaa/Ceas Aeroacoustics Conference and Exhibit. |
0.356 |
|
| 2001 |
Saha N, Ma R, Devenport WJ. Characterizing unsteady periodic disturbances in the tip leakage vortex of an idealized axial compressor rotor blade 39th Aerospace Sciences Meeting and Exhibit. |
0.46 |
|
| 2000 |
Glegg S, Devenport W. Methods for calculating the response of structures to inhomogeneous turbulent flows Journal of the Acoustical Society of America. 107: 2823-2823. DOI: 10.1121/1.429110 |
0.476 |
|
| 2000 |
Glegg SAL, Devenport WJ. Compact eddy structures and their application to aero acoustics 6th Aeroacoustics Conference and Exhibit. |
0.431 |
|
| 2000 |
Ma R, Saha N, Devenport WJ, Wang Y. Unsteady behavior of a tip leakage vortex produced by simulated stator/rotor interaction Fluids 2000 Conference and Exhibit. |
0.441 |
|
| 2000 |
Muthanna C, De Riva DL, Devenport WJ, Glegg SAL. The interaction of free-stream Turbulence with a compressor cascade Fluids 2000 Conference and Exhibit. |
0.445 |
|
| 1999 |
Glegg SAL, Devenport WJ, Wittmer KS, Pope DS. Broadband helicopter noise generated by blade wake interactions Journal of the American Helicopter Society. 44: 293-301. DOI: 10.4050/Jahs.44.293 |
0.58 |
|
| 1999 |
Wittmer KS, Devenport WJ, Wenger CW. Turbulence structure resulting from a vortex/wing-tip encounter Journal of the American Helicopter Society. 44: 141-149. DOI: 10.4050/Jahs.44.141 |
0.591 |
|
| 1999 |
Wenger CW, Devenport WJ. Seven-hole pressure probe calibration method utilizing look-up error tables Aiaa Journal. 37: 675-679. DOI: 10.2514/2.794 |
0.413 |
|
| 1999 |
Wittmer KS, Devenport WJ, Glegg SAL. Effects of perpendicular blade-vortex interaction, Part 2: parameter study Aiaa Journal. 37: 813-817. DOI: 10.2514/2.7528 |
0.54 |
|
| 1999 |
Wittmer KS, Devenport WJ. Effects of perpendicular blade-vortex interaction, Part 1: turbulence structure and development Aiaa Journal. 37: 805-812. DOI: 10.2514/2.7527 |
0.557 |
|
| 1999 |
Devenport WJ, Vogel CM, Zsoldos JS. Flow structure produced by the interaction and merger of a pair of co-rotating wing-tip vortices Journal of Fluid Mechanics. 394: 357-377. DOI: 10.1017/S0022112099005777 |
0.457 |
|
| 1999 |
Bereketab S, Devenport WJ. Complex equilibrium of laterally curved wakes 37th Aerospace Sciences Meeting and Exhibit. |
0.335 |
|
| 1999 |
Shin S, Ragab SA, Devenport WJ. Numerical simulation of highly staggered cascade flow using an unstructured grid 30th Fluid Dynamics Conference. |
0.355 |
|
| 1998 |
Wenger CW, Devenport WJ, Wittmer KS, Muthanna C. Two-point measurements in the wake of a compressor cascade 29th Aiaa Fluid Dynamics Conference. 1-12. DOI: 10.2514/6.1998-2556 |
0.452 |
|
| 1998 |
Miranda JA, Devenport WJ. Turbulence structure in the spiral wake shed by a lifting wing Aiaa Journal. 36: 658-660. DOI: 10.2514/2.421 |
0.42 |
|
| 1998 |
Wittmer KS, Devenport WJ, Zsoldos JS. A four-sensor hot-wire probe system for three-component velocity measurement Experiments in Fluids. 24: 416-423. DOI: 10.1007/S003480050191 |
0.406 |
|
| 1998 |
Wenger CW, Devenport WJ. A seven hole pressure probe measurement system and calffiration method utilizing error tables 36th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.363 |
|
| 1998 |
Muthanna C, Wittmer KS, Devenport WJ. Turbulence structure of the flow downstream of a compressor cascade with tip leakage 36th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.391 |
|
| 1998 |
Devenport WJ, Wenger CW, Glegg SAL, Miranda JA. Wave number frequency spectra of a lifting wake for broadband noise prediction Aiaa Journal. 36: 881-887. |
0.389 |
|
| 1998 |
Goody MC, Simpson RL, Engel M, Chesnakas CJ, Devenport WJ. Mean velocity and pressure and velocity spectral measurements within a separated flow around a prolate spheroid at incidence 36th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.428 |
|
| 1998 |
Youssef KS, Ragab SA, Devenport WJ, Abdel Gawad AF. Large eddy simulation of the near wake of a rectangular wing 36th Aiaa Aerospace Sciences Meeting and Exhibit. |
0.373 |
|
| 1997 |
Devenport WJ, Wenger CW, Glegg SAL, Miranda JA. Wavenumber frequency spectra of turbulence in a lifting wake for broadband noise prediction 3rd Aiaa/Ceas Aeroacoustics Conference. 826-836. DOI: 10.2514/6.1997-1699 |
0.472 |
|
| 1997 |
Devenport WJ, Zsoldos JS, Vogel CM. The structure and development of a counter-rotating wing-tip vortex pair Journal of Fluid Mechanics. 332: 71-104. DOI: 10.1017/S0022112096003795 |
0.509 |
|
| 1997 |
Wittmer KS, Devenport WJ, Wenger CW. Turbulence structure resulting from a vortex/blade-tip interaction 35th Aerospace Sciences Meeting and Exhibit. |
0.484 |
|
| 1997 |
Devenport WJ, Wittmer KS, Muthanna C, Bereketab S, Moore J. Turbulence structure of a tip-leakage vortex wake 35th Aerospace Sciences Meeting and Exhibit. |
0.455 |
|
| 1996 |
Devenport WJ, Rife MC, Liapis SI, Follin GJ. The structure and development of a wing-tip vortex Journal of Fluid Mechanics. 312: 67-106. DOI: 10.1017/S0022112096001929 |
0.512 |
|
| 1996 |
Miranda JA, Devenport WJ. Two-point measurements in trailing vortices 34th Aerospace Sciences Meeting and Exhibit. |
0.326 |
|
| 1996 |
Wittmer KS, Devenport WJ. Turbulence structure resulting from a perpendicular airfoil-vortex interaction 1996 Fluid Dynamics Conference. 1-11. |
0.444 |
|
| 1995 |
Wittmer KS, Devenport WJ, Rife MC, Glegg SAL. Perpendicular blade vortex interaction Aiaa Journal. 33: 1667-1674. DOI: 10.2514/3.12802 |
0.529 |
|
| 1995 |
Wittmer KS, Devenport WJ. Interaction of a streamwise vortex with a full-span blade 1995 Fluid Dynamics Conference. 1-11. |
0.394 |
|
| 1995 |
Devenport WJ, Rife MC, Liapis SI, Follin GJ. Turbulence structure and scaling in trailing vortices 33rd Aerospace Sciences Meeting and Exhibit. |
0.416 |
|
| 1994 |
Devenport WJ, Smith EJ. The diode-array velocimeter Journal of Fluid Mechanics. 259: 167-189. DOI: 10.1017/S002211209400008X |
0.485 |
|
| 1993 |
Devenport WJ, Sutton EP. An experimental study of two flows through an axisymmetric sudden expansion Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow. 14: 423-432. DOI: 10.1007/Bf00190197 |
0.505 |
|
| 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 |
0.5 |
|
| 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 |
0.467 |
|
| 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 |
0.495 |
|
| 1991 |
Devenport WJ, Sutton EP. Near-Wall Behavior of Separated and Reattaching Flows Aiaa Journal. 29: 25-31. DOI: 10.2514/3.10541 |
0.515 |
|
| 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 |
0.439 |
|
| 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 |
0.541 |
|
| 1990 |
Devenport WJ, Evans GP, Sutton EP. A traversing pulsed-wire probe for velocity measurements near a wall Experiments in Fluids. 8: 336-342. DOI: 10.1007/Bf00217198 |
0.453 |
|
| 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. |
0.329 |
|
| 1986 |
Devenport WJ, Simpson RL. SOME TIME-DEPENDENT FEATURES OF TURBULENT APPENDAGE-BODY JUNCTURE FLOWS . 312-335. |
0.409 |
|
| Show low-probability matches. |