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Joseph A. Schetz - Publications

Affiliations: 
Virginia Polytechnic Institute and State University, Blacksburg, VA, United States 
Area:
Aerospace Engineering, Fluid and Plasma Physics
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164 high-probability publications. We are testing a new system for linking publications to authors. You can help! If you notice any inaccuracies, please sign in and mark papers as correct or incorrect matches. If you identify any major omissions or other inaccuracies in the publication list, please let us know.

Year Citation  Score
2020 Massa L, Schetz JA. Hypersonic Heat Flux Reconstruction with Distributed Temperature Sensors Journal of Thermophysics and Heat Transfer. 34: 331-346. DOI: 10.2514/1.T5778  0.332
2019 Vincent TG, Rolfe EN, Lowe KT, Schetz JA. Aerodynamic Analysis of Total Temperature Probe Thermal Performance Using Conjugate Heat Transfer Journal of Thermophysics and Heat Transfer. 33: 830-843. DOI: 10.2514/1.T5635  0.394
2018 Mallik W, Schetz JA, Kapania RK. Rapid Transonic Flutter Analysis for Aircraft Conceptual Design Applications Aiaa Journal. 56: 2389-2402. DOI: 10.2514/1.J056218  0.334
2017 Mallik W, Kapania RK, Schetz JA. Aeroelastic Applications of a Variable-Geometry Raked Wingtip Journal of Aircraft. 54: 62-74. DOI: 10.2514/1.C033805  0.372
2017 Meritt RJ, Schetz JA, Marineau EC, Lewis DR, Daniel DT. Direct Skin Friction Measurements at Mach 10 in a Hypervelocity Wind Tunnel Journal of Spacecraft and Rockets. 54: 871-882. DOI: 10.2514/1.A33657  0.738
2016 Meritt RJ, Schetz JA. Skin friction sensor development, validation, and application for high-speed, high-enthalpy flow conditions Journal of Propulsion and Power. 32: 821-833. DOI: 10.2514/1.B35917  0.454
2016 Segee MC, Schetz JA, Kapania RK. Transonic aerodynamics analysis for multidisciplinary design optimization applications 34th Aiaa Applied Aerodynamics Conference.  0.302
2015 Meritt RJ, Schetz JA, Marineau EC, Lewis DR. Direct measurements of skin friction at AEDC hypervelocity wind tunnel 9 53rd Aiaa Aerospace Sciences Meeting. DOI: 10.2514/6.2015-1914  0.751
2015 Chakraborty I, Nam T, Gross JR, Mavris DN, Schetz JA, Kapania RK. Comparative assessment of strut-braced and truss-braced wing configurations using multidisciplinary design optimization Journal of Aircraft. 52: 2009-2020. DOI: 10.2514/1.C033120  0.331
2015 Mallik W, Kapania RK, Schetz JA. Effect of flutter on the multidisciplinary design optimization of truss-braced-wing aircraft Journal of Aircraft. 52: 1858-1872. DOI: 10.2514/1.C033096  0.339
2015 Mallik W, Kapania RK, Schetz JA. Transonic aeroelastic analysis for multidisciplinary design optimization applications 57th Aiaa/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference.  0.304
2014 Meritt RJ, Schetz JA, Donbar JM, Tam CJ. Skin friction sensor for high-speed, high-enthalpy scramjet flow applications 50th Aiaa/Asme/Sae/Asee Joint Propulsion Conference 2014. DOI: 10.2514/6.2014-3942  0.378
2014 Shirley CM, Schetz JA, Kapania RK, Haftka RT. Tradeoffs of wing weight and lift/drag in design of medium-range transport aircraft Journal of Aircraft. 51: 904-912. DOI: 10.2514/1.C032605  0.376
2014 Morris CC, Allison DL, Schetz JA, Kapania RK, Sultan C. Parametric geometry model for design studies of tailless supersonic aircraft Journal of Aircraft. 51: 1455-1466. DOI: 10.2514/1.C032340  0.305
2014 Meritt RJ, Schetz JA. Skin friction sensor validation for high-speed, high-enthalpy flow applications Aiaa Aviation 2014 - 30th Aiaa Aerodynamic Measurement Technology and Ground Testing Conference.  0.346
2013 Leifsson L, Ko A, Mason WH, Schetz JA, Grossman B, Haftka RT. Multidisciplinary design optimization of blended-wing-body transport aircraft with distributed propulsion Aerospace Science and Technology. 25: 16-28. DOI: 10.1016/J.Ast.2011.12.004  0.391
2012 Kush EA, Schetz JA. Liquid Jet Injection into a Supersonic Flow Aiaa Journal. 11: 1223-1224. DOI: 10.2514/3.50567  0.417
2012 Peraudo PN, Schetz JA, Roy CJ. Computational study of the embedded engine static pressure thrust propulsion system 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.2514/1.C031840  0.5
2012 Knight KCD, Braun EM, Roy CJ, Lu FK, Schetz JA. Interference drag modeling and experiments for a high-reynolds-number transonic wing Journal of Aircraft. 49: 1894-1903. DOI: 10.2514/1.C031731  0.512
2012 Meadows NA, Schetz JA, Kapania RK, Bhatia M, Seber G. Multidisciplinary design optimization of medium-range transonic truss-braced wing transport aircraft Journal of Aircraft. 49: 1844-1856. DOI: 10.2514/1.C031695  0.303
2011 Gur O, Schetz JA, Mason WH. Aerodynamic considerations in the design of truss-braced-wing aircraft Journal of Aircraft. 48: 919-939. DOI: 10.2514/1.C031171  0.454
2011 Duggirala RK, Roy CJ, Schetz JA. Analysis of interference drag for strut-strut interaction in transonic flow Aiaa Journal. 49: 449-462. DOI: 10.2514/1.45703  0.52
2011 Gur O, Bhatia M, Mason WH, Schetz JA, Kapania RK, Nam T. Development of a framework for truss-braced wing conceptual MDO Structural and Multidisciplinary Optimization. 44: 277-298. DOI: 10.1007/S00158-010-0612-9  0.323
2011 Rock C, Schetz JA, Ungewitter R. Experimental and numerical studies of injector array configurations for circular scramjet combustors 41st Aiaa Fluid Dynamics Conference and Exhibit.  0.328
2011 Knight KCD, Braun EM, Roy CJ, Lu FK, Schetz JA. Interference drag modeling and experiments for a high reynolds number transonic wing 29th Aiaa Applied Aerodynamics Conference 2011.  0.45
2010 Schetz JA, Maddalena L, Burger SK. Molecular weight and shock-wave effects on transverse injection in supersonic flow Journal of Propulsion and Power. 26: 1102-1113. DOI: 10.2514/1.49355  0.703
2010 Gur O, Bhatia M, Schetz JA, Mason WH, Kapania RK, Mavris DN. Design optimization of a truss-braced-wing transonic transport aircraft Journal of Aircraft. 47: 1907-1917. DOI: 10.2514/1.47546  0.386
2010 Hosder S, Schetz JA, Mason WH, Grossman B, Haftka RT. Computational-fluid-dynamics-based clean-wing aerodynamic noise model for design Journal of Aircraft. 47: 754-762. DOI: 10.2514/1.29105  0.321
2010 Schetz JA, Hosder S, Dippold V, Walker J. Propulsion and aerodynamic performance evaluation of jet-wing distributed propulsion Aerospace Science and Technology. 14: 1-10. DOI: 10.1016/J.Ast.2009.06.010  0.489
2010 Schetz JA. Direct measurement of skin friction in complex flows 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.  0.305
2010 Rock C, Schetz JA, Ungewitter R. Injectant molecular weight effects in injectors for circular scramjet combustors 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.  0.389
2010 Throckmorton R, Schetz JA, Jacobsen LS. Experimental and computational investigation of a dynamic starting method for supersonic/hypersonic inlets 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.  0.407
2010 Gur O, Schetz JA, Mason WH. Aerodynamic considerations in the design of truss-braced wing aircraft 28th Aiaa Applied Aerodynamics Conference.  0.375
2009 Gur O, Mason WH, Schetz JA. Full configuration drag estimation Collection of Technical Papers - Aiaa Applied Aerodynamics Conference. DOI: 10.2514/1.47557  0.412
2009 Scott KML, McQuigg TD, Mulani SB, Kapania RK, Schetz JA. Flow induced vibrations of pressure/temperature sensors Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. DOI: 10.2514/1.45016  0.345
2009 Marineau EC, Schetz JA, Neel RE. Computational and experimental investigation of supersonic convection over a laser-heated target Journal of Thermophysics and Heat Transfer. 23: 502-512. DOI: 10.2514/1.33697  0.709
2009 Viti V, Neel R, Schetz JA. Detailed flow physics of the supersonic jet interaction flow field Physics of Fluids. 21. DOI: 10.1063/1.3112736  0.468
2009 Rock C, Schetz JA, Ungewitter R. Experimental and numerical studies of a strut injector for round scramjet combustors 16th Aiaa/Dlr/Dglr International Space Planes and Hypersonic Systems and Technologies Conference.  0.444
2009 Rock C, Duchmann A, Schetz JA, Ungewitter R. Studies of a wall injector array for circular high-mach-number combustors 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.  0.356
2008 Schetz JA, Maddalena L, Throckmorton R, Neel R. Complex wall injector array for high-speed combustors Journal of Propulsion and Power. 24: 673-680. DOI: 10.2514/1.36660  0.71
2008 Grossman PM, Maddalena L, Schetz JA. Flush-wall, diamond-shaped fuel injector for high Mach number scramjets Journal of Propulsion and Power. 24: 259-266. DOI: 10.2514/1.29956  0.676
2008 Bonanos AM, Schetz JA, O'Brien WF, Goyne CP. Dual-mode combustion experiments with an integrated aeroramp-injector/ plasma-torch igniter Journal of Propulsion and Power. 24: 267-273. DOI: 10.2514/1.28301  0.761
2008 Maddalena L, Schetz JA, Neel R. Vortex interactions with a jet in a supersonic crossflow 46th Aiaa Aerospace Sciences Meeting and Exhibit.  0.58
2008 Maddalena L, Shafer TC, Schetz JA. Studies of the detailed vortical structures in a jet in a supersonic crossflow 46th Aiaa Aerospace Sciences Meeting and Exhibit.  0.686
2008 Schetz JA, Maddalena L, Throckmorton R, Neel R. Complex wall injector array for scramjet combustors 46th Aiaa Aerospace Sciences Meeting and Exhibit.  0.543
2007 Marineau EC, Schetz JA, Neel RE. Turbulent navier-stokes simulations of heat transfer with complex wall temperature variations Journal of Thermophysics and Heat Transfer. 21: 525-535. DOI: 10.2514/1.26007  0.722
2007 Campioli TL, Schetz JA. Assessment of reacting and non-reacting supersonic mixing 2007 Proceedings of the 5th Joint Asme/Jsme Fluids Engineering Summer Conference, Fedsm 2007. 1: 1835-1841. DOI: 10.1115/FEDSM2007-37166  0.812
2007 Marineau EC, Schetz JA, Neel RE. Computational and experimental investigation of supersonic convection over a laser heated target Collection of Technical Papers - 39th Aiaa Thermophysics Conference. 1: 564-580.  0.663
2006 Orr MW, Schetz JA, Fielder RS. Fiber-optic wall shear gauge for hot high-speed flows Aiaa Journal. 44: 1158-1168. DOI: 10.2514/1.8373  0.392
2006 Maddalena L, Campioli TL, Schetz JA. Experimental and computational investigation of light-gas injectors in Mach 4.0 crossflow Journal of Propulsion and Power. 22: 1027-1038. DOI: 10.2514/1.19141  0.814
2006 Rolling AJ, Schetz JA. Direct skin friction measurements with shock-impingement compensation in complex turbulent flows Collection of Technical Papers - 25th Aiaa Aerodynamic Measurement Technology and Ground Testing Conference. 2: 1240-1252.  0.813
2006 Grossman P, Maddalena L, Schetz JA. Wall injectors for high mach number scramjets Collection of Technical Papers - Aiaa/Asme/Sae/Asee 42nd Joint Propulsion Conference. 5: 3606-3615.  0.58
2006 Campioli TL, Maddalena L, Schetz JA. Studies of shock wave/transverse injection interaction on supersonic mixing processes A Collection of Technical Papers - 14th Aiaa/Ahi International Space Planes and Hypersonic Systems and Technologies Conference. 3: 2270-2294.  0.812
2006 Sang AK, Rolling AJ, Schetz JA. A novel skin friction sensor for hypersonic flow Collection of Technical Papers - 25th Aiaa Aerodynamic Measurement Technology and Ground Testing Conference. 2: 1233-1239.  0.81
2006 Billingsley MC, O'Brien WF, Schetz JA. Plasma torch atomizer-igniter for supersonic combustion of liquid hydrocarbon fuels A Collection of Technical Papers - 14th Aiaa/Ahi International Space Planes and Hypersonic Systems and Technologies Conference. 1: 615-630.  0.335
2006 Bonanos AM, Schetz JA, Brien WFO, Goyne CP. Integrated aeroramp-injector/plasma-torch igniter for methane and ethylene fueled scramjets Collection of Technical Papers - 44th Aiaa Aerospace Sciences Meeting. 13: 9753-9759.  0.735
2005 Byun YH, Bae KJ, Wallis S, Viti V, Schetz JA, Bowersox R. Jet interaction in supersonic flow with a downstream surface ramp Journal of Spacecraft and Rockets. 42: 38-44. DOI: 10.2514/1.4021  0.497
2005 Andersen CD, Schetz JA. Liquid-fuel aeroramp injector for scramjets Journal of Propulsion and Power. 21: 371-374. DOI: 10.2514/1.12238  0.385
2005 Schetz JA. Skin Friction Measurements in Complex Turbulent Flows Using Direct Methods Engineering Turbulence Modelling and Experiments 6. 421-430. DOI: 10.1016/B978-008044544-1/50040-6  0.322
2005 Maddalena L, Campioli TL, Schetz JA. Experimental and computational investigation of an aeroramp injector in a mach four cross flow A Collection of Technical Papers - 13th Aiaa/Cira International Space Planes and Hypersonic Systems and Technologies Conference. 1: 287-302.  0.818
2005 Bonanos AM, Schetz JA, O'Brien WF, Goyne CP. Scramjet operability range studies of a multifuel integrated aeroramp injector/plasma igniter A Collection of Technical Papers - 13th Aiaa/Cira International Space Planes and Hypersonic Systems and Technologies Conference. 3: 1980-1990.  0.755
2005 Byun YH, Bae KJ, Wallis S, Viti V, Schetz JA, Bowersox R. Jet interaction in supersonic flow with a downstream surface ramp Journal of Spacecraft and Rockets. 42: 38-44.  0.398
2004 Byun Y, Bae K, Schetz JA, Lee J. A Study for Performance Enhancement of Side Jet using a Ramp Journal of the Korean Society For Aeronautical & Space Sciences. 32: 73-79. DOI: 10.5139/Jksas.2004.32.4.073  0.491
2004 Viti V, Wallis S, Schetz JA, Neel R, Bowersox RDW. Jet interaction with a primary jet and an array of smaller jets Aiaa Journal. 42: 1358-1368. DOI: 10.2514/1.4850  0.481
2003 Gallimore SD, Jacobsen LS, O'Brien WF, Schetz JA. Operational sensitivities of an integrated scramjet ignition/fuel-injection system Journal of Propulsion and Power. 19: 183-189. DOI: 10.2514/2.6116  0.378
2003 Jacobsen LS, Gallimore SD, Schetz JA, O'Brien WF. Integration of an aeroramp injector/plasma igniter for hydrocarbon scramjets Journal of Propulsion and Power. 19: 170-182. DOI: 10.2514/2.6114  0.451
2003 Tomioka S, Jacobsen LS, Schetz JA. Modified mixing analogy for studies of mixing in supersonic flows Journal of Propulsion and Power. 19: 151-154. DOI: 10.2514/2.6093  0.422
2003 Tomioka S, Jacobsen LS, Schetz JA. Sonic injection from diamond-shaped orifices into a supersonic crossflow Journal of Propulsion and Power. 19: 104-114. DOI: 10.2514/2.6086  0.441
2003 Smith TB, Schetz JA, Bui TT. Development of direct-measuring skin-friction gauges for hypersonic flight tests Aiaa Journal. 41: 1429-1437. DOI: 10.2514/2.2125  0.451
2003 MacLean M, Schetz JA. Numerical study of detailed flow affecting a direct measuring skin-friction gauge Aiaa Journal. 41: 1271-1281. DOI: 10.2514/2.2095  0.66
2003 Anderson C, Schetz JA, O'Brien WF. Integrated liquid-fuel-injector/plasma-igniter for scramjets 12th Aiaa International Space Planes and Hypersonic Systems and Technologies.  0.34
2003 Magill SA, Schetz JA, Mason WH. Compound aircraft transport: A comparison of vvingtip-docked and close-formation flight 41st Aerospace Sciences Meeting and Exhibit.  0.776
2003 Bonanos AM, Sanders DD, Schetz JA, O'Brien WF, Goyne CP, Krauss RH, McDaniel JC. Hot-flow testing of an integrated aero-ramp-injector/plasma-ingiter for scramjets with hydrogen and hydrocarbon fuels 12th Aiaa International Space Planes and Hypersonic Systems and Technologies.  0.751
2003 Jacobsen LS, Gallimore SD, Schetz JA, O'Brien WF, Goss LP. Improved aerodynamic-ramp injector in supersonic flow Journal of Propulsion and Power. 19: 663-673.  0.45
2002 Magill S, MacLean M, Schetz J, Kapania R, Sang A, Pulliam W. Study of Direct-Measuring Skin-Friction Gauge with Rubber Sheet for Damping Aiaa Journal. 40: 50-57. DOI: 10.2514/2.1640  0.763
2002 Smith TB, Schetz JA, Bui TT. Development and ground testing of direct measuring skin friction gages for high enthalpy supersonic flight tests 22nd Aiaa Aerodynamic Measurement Technology and Ground Testing Conference.  0.367
2001 Tetrault P, Schetz JA, Grossman B. Numerical Prediction of Interference Drag of Strut-Surface Intersection in Transonic Flow Aiaa Journal. 39: 857-864. DOI: 10.2514/2.1389  0.779
2001 Jacobsen LS, Gallimore SD, Schetz JA, O'Brien WF, Goss LP. An integrated aeroramp injector/plasma-igniter for hydrocarbon fuels in a supersonic flow: Part A: Experimental studies of the geometric configuration 10th Aiaa/Nal-Nasda-Isas International Space Planes and Hypersonic Systems and Technologies Conference.  0.355
2001 Jacobsen LS, Gallimore SD, Schetz JA, O'Brien WF, Goss LP. An improved aerodynamic ramp injector in supersonic flow 39th Aerospace Sciences Meeting and Exhibit.  0.463
2001 Orr M, Magill SA, Schetz JA, Marchman IF, Mason WH, Grossman B. Experimental study of the aerodynamic properties of the inboard wing concept 39th Aerospace Sciences Meeting and Exhibit.  0.806
2000 Jacobsen LS, Schetz JA, Ng WF. Flowfield near a multiport injector array in a supersonic flow Journal of Propulsion and Power. 16: 216-226. DOI: 10.2514/2.5586  0.517
2000 Gundlach JF, Tetrault P, Gern FH, Nagshineh-Pour AH, Ko A, Schetz JA, Mason WH, Kapania RK, Grossman B, Haftka RT. Conceptual Design Studies of a Strut-Braced Wing Transonic Transport Journal of Aircraft. 37: 976-983. DOI: 10.2514/2.2724  0.774
2000 Remington A, Schetz JA. A study of magnetically damped skin friction measurements for high vibration environments 21st Aerodynamic Measurement Technology and Ground Testing Conference.  0.31
2000 Tétrault PA, Schetz JA, Grossman B. Numerical prediction of the interference drag of a streamlined strut intersecting a surface in transonic flow 38th Aerospace Sciences Meeting and Exhibit.  0.391
2000 Tomioka S, Jacobsen LS, Schetz JA. Interaction between a supersonic airstream and a sonic jet injected through a diamond-shaped orifice 38th Aerospace Sciences Meeting and Exhibit.  0.352
2000 Smith TB, Schetz JA, Bui TT. Direct skin friction measurement in a rocket-based-combined-cycle scramjet combustor 36th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit.  0.339
2000 Gundlach IV JF, Tétrault PA, Gern FH, Nagshineh-Pour AH, Ko A, Schetz JA, Mason WH, Kapania RK, Grossman B, Haftka RT. Conceptual design studies of a strut-braced wing transonic transport Journal of Aircraft. 37: 976-983.  0.319
2000 Smith TB, Schetz JA, Bui TT. Direct skin friction measurement in a rocket-based-combined-cycle scramjet combustor 36th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit.  0.339
1999 Gern FH, Gundlach JF, Ko A, Naghshineh-Pour A, Sulaeman E, Tetrault PA, Grossman B, Kapania RK, Mason WH, Schetz JA, Haftka RT. Multidisciplinary design optimization of a transonic commercial transport with a strut-braced wing Sae Technical Papers. DOI: 10.4271/1999-01-5621  0.763
1999 Wesner A, Schetz JA, Grabowski H. Interferometric study of unsteady passing shock flow in a turbine cascade Journal of Propulsion and Power. 15: 489-496. DOI: 10.2514/2.5463  0.432
1999 Jacobsen LS, Schetz JA, Gallimore SD, O'Brien WF. Mixing enhancement by jet swirl in a multiport injector array in supersonic flow Proceedings of the 1999 3rd Asme/Jsme Joint Fluids Engineering Conference, Fedsm'99, San Francisco, California, Usa, 18-23 July 1999 (Cd-Rom). 1.  0.444
1999 Xillo OC, Schetz JA, Ng WF. A sampling probe for fluctuating concentration measurements in supersonic flow 37th Aerospace Sciences Meeting and Exhibit.  0.317
1998 Fuller RP, Wu PK, Nejad AS, Schetz JA. Comparison of physical and aerodynamic ramps as fuel injectors in supersonic flow Journal of Propulsion and Power. 14: 135-145. DOI: 10.2514/2.5278  0.444
1998 Schetz JA. Turbulent Shear Layers in Supersonic Flow Aiaa Journal. 36: 879-880. DOI: 10.2514/2.455  0.398
1998 Jacobsen LS, Schetz JA, Ng WF. The flowfield near a multiport injector array in a supersonic flow 34th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit.  0.442
1997 Barber MJ, Schetz JA, Roe LA. Normal, Sonic Helium Injection Through a Wedge-Shaped Orifice into Supersonic Flow Journal of Propulsion and Power. 13: 257-263. DOI: 10.2514/2.5157  0.427
1997 Lewis DP, Schetz JA. Tangential injection from overlaid slots into a supersonic stream Journal of Propulsion and Power. 13: 59-63. DOI: 10.2514/2.5150  0.423
1997 Schetz JA. Direct Measurement of Skin Friction in Complex Fluid Flows Applied Mechanics Reviews. 50. DOI: 10.1115/1.3101835  0.488
1997 Hytopoulos E, Schetz JA, Simpson RL. Turbulence model for steady and unsteady boundary layers in strong pressure gradients Journal of Fluids Engineering, Transactions of the Asme. 119: 541-549.  0.324
1997 Wesner A, Schetz JA, Grabowski H. An interferometric study of unsteady passing shock flow in a turbine cascade 33rd Joint Propulsion Conference and Exhibit.  0.339
1997 Novean MG, Schetz JA, Bowersox RDW. Direct measurements of skin friction in complex supersonic flows 35th Aerospace Sciences Meeting and Exhibit.  0.405
1997 Wilt JA, Tyll JS, Schetz JA, Marchman JF. Aerodynamic performance of an electrodynamic suspension MagLev vehicle 35th Aerospace Sciences Meeting and Exhibit. 1-14.  0.321
1996 Liu DJ, Marshakov A, Marchman JF, Schetz JA. Aerodynamic evaluation of two maglev designs Sae Technical Papers. DOI: 10.4271/960905  0.307
1996 Marshakov AV, Schetz JA, Kiss T. Direct measurement of skin friction in a turbine cascade Journal of Propulsion and Power. 12: 245-249. DOI: 10.2514/3.24020  0.485
1996 Tyll JS, Liu D, Schetz JA, Marchman JF. Experimental studies of magnetic levitation train aerodynamics Aiaa Journal. 34: 2465-2470. DOI: 10.2514/3.13425  0.432
1996 Kiss T, Schetz JA, Moses HL. Experimental and numerical study of transonic turbine cascade flow Aiaa Journal. 34: 104-109. DOI: 10.2514/3.13028  0.497
1996 Tyll JS, Liu D, Schetz JA, Marchman JF. Experimental studies of magnetic levitation train aerodynamics Aiaa Journal. 34: 2465-2470.  0.321
1996 King PS, Schetz JA. Interaction of jets and shear layers to produce instabilities and mixing enhancement in supersonic flows 34th Aerospace Sciences Meeting and Exhibit.  0.338
1995 Bowersox RDW, Schetz JA. Measurements of compressible turbulent flow structure in a supersonic mixing layer Aiaa Journal. 33: 2101-2106. DOI: 10.2514/3.12953  0.458
1995 Bowersox RDW, Schetz JA, Chadwick K, Deiwert S. Technique for direct measurement of skin friction in high enthalpy impulsive scramjet flowfields Aiaa Journal. 33: 1286-1291. DOI: 10.2514/3.12677  0.417
1995 Bowersox RD, Schetz JA, Conners RW. Digital analysis of shadowgraph images for statistical index of refraction (density) turbulent fluctuation properties in high-speed flow Measurement. 15: 201-209. DOI: 10.1016/0263-2241(95)00004-5  0.431
1994 Arai T, Schetz JA. Injection of bubbling liquid jets from multiple injectors into a supersonic stream Journal of Propulsion and Power. 10: 382-386. DOI: 10.2514/3.23746  0.444
1994 Bowersox RDW, Schetz JA. Model for compressible turbulence in hypersonic wall boundary and high-speed mixing layers Aiaa Journal. 32: 1531-1533. DOI: 10.2514/3.12224  0.425
1994 Bowersox RDW, Schetz JA. Compressible turbulence measurements in a high-speed high-Reynolds-number mixing layer Aiaa Journal. 32: 758-764. DOI: 10.2514/3.12050  0.431
1993 Kiss T, Schetz JA. Rational extension of the Clauser eddy viscosity model to compressible boundary-layer flow Aiaa Journal. 31: 1007-1013. DOI: 10.2514/3.11722  0.361
1992 Fuller EJ, Mays RB, Thomas RH, Schetz JA. Mixing studies of helium in air at high supersonic speeds Aiaa Journal. 30: 2234-2243. DOI: 10.2514/3.11210  0.41
1992 Caille J, Schetz JA. Three-dimensional strip-integral method for incompressible turbulent boundary layers Aiaa Journal. 30: 1207-1213. DOI: 10.2514/3.11052  0.392
1991 King PS, Thomas RH, Schetz JA, Billig FS. Combined tangential-normal injection into a supersonic flow Journal of Propulsion and Power. 7: 420-430. DOI: 10.2514/3.23343  0.502
1991 Thomas RH, Schetz JA, Pelletier DH. Three-dimensional finite element method analysis of turbulent flow over self-propelled slender bodies Journal of Propulsion and Power. 7: 281-287. DOI: 10.2514/3.23322  0.433
1991 Caille J, Schetz JA. New wall treatment for numerical Navier-Stokes solution of incompressible turbulent flows Aiaa Journal. 31: 20-26. DOI: 10.2514/3.11313  0.428
1991 Situ M, Schetz JA. New mixing-length model for turbulent high-speed flows Aiaa Journal. 29: 872-873. DOI: 10.2514/3.10670  0.476
1990 Oh TS, Schetz JA. Finite Element Simulation of Complex Jets in a Crossflow for V/STOL Applications Journal of Aircraft. 27: 389-399. DOI: 10.2514/3.25288  0.481
1990 Hyde CR, Smith BR, Schetz JA, Walker DA. Turbulence measurements for heated gas slot injection in supersonic flow Aiaa Journal. 28: 1605-1614. DOI: 10.2514/3.25259  0.454
1990 Clark RL, Ng WF, Walker DA, Schetz JA. Large-Scale Structure in a Supersonic Slot-Injected Flowfield Aiaa Journal. 28: 1045-1051. DOI: 10.2514/3.25163  0.398
1990 Kwok FT, Andrew PL, Ng WF, Schetz JA. Experimental Investigation of a Supersonic Shear Layer with Slot Injection of Helium Aiaa Journal. 29: 1426-1435. DOI: 10.2514/3.10756  0.365
1989 Kavsaoglu MS, Schetz JA, Jakubowski AK. Rectangular jets in a crossflow Journal of Aircraft. 26: 793-804. DOI: 10.2514/3.45843  0.447
1989 Kavsaoglu MS, Schetz JA. Effects of swirl and high turbulence on a jet in a crossflow Journal of Aircraft. 26: 539-546. DOI: 10.2514/3.45800  0.446
1988 Schetz JA, Pelletier D, Mallory DA. Experimental and numerical investigation of a propeller with three-dimensional inflow Journal of Propulsion and Power. 4: 341-349. DOI: 10.2514/3.23072  0.478
1987 Caille J, Schetz JA. Finite element Navier-Stokes analysis of the flow about a finite plate Aiaa Journal. 27: 1089-1096. DOI: 10.2514/3.10226  0.416
1986 Less DM, Schetz JA. Transient Behavior of Liquid Jets Injected Normal to a High-Velocity Gas Stream Aiaa Journal. 24: 1979-1986. DOI: 10.2514/3.9556  0.423
1986 Pelletier DH, Schetz JA. Finite element Navier-Stokes calculation of three-dimensional turbulent flow near a propeller Aiaa Journal. 24: 1409-1416. DOI: 10.2514/3.9457  0.319
1986 Kotb MA, Schetz JA. Measurements of three-dimensional turbulent flow behind a propeller in a shear flow Aiaa Journal. 24: 570-577. DOI: 10.2514/3.9309  0.467
1985 Thomas RH, Schetz JA. Distributions across the plume of transverse liquid and slurry jets in supersonic airflow Aiaa Journal. 23: 1892-1901. DOI: 10.2514/3.9193  0.418
1985 Situ M, Schetz JA. Computational and experimental study of the effect of mass transfer on liquid-jet breakup Aiaa Journal. 23: 254-261. DOI: 10.2514/3.8903  0.334
1985 Lee H, Schetz JA. Experimental results for Reynolds number effects on trailing vortices Journal of Aircraft. 22: 158-160. DOI: 10.2514/3.45101  0.466
1985 Schetz JA, Guruswamy J, Marchman JF. Effects of an S-Inlet on the Flow in a Dump Combustor Journal of Spacecraft and Rockets. 22: 221-224. DOI: 10.2514/3.25738  0.392
1984 Schetz JA, Jakubowski AK, Aoyagi K. Surface pressures on a flat plate with dual jet configurations Journal of Aircraft. 21: 484-490. DOI: 10.2514/3.44997  0.303
1983 Hewitt PW, Schetz JA. Transverse Jet Break-up and Atomization with Rapid Vaporization along the Trajectory. Aiaa Journal. 23: 596-603. DOI: 10.2514/3.8956  0.483
1983 Ogg JC, Schetz JA. Breakup and droplet formation of slurry jets Aiaa Journal. 23: 432-439. DOI: 10.2514/3.8931  0.341
1983 Schetz JA, Hewitt PW, Thomas R. Swirl combustor flow visualization studies in a water tunnel Journal of Spacecraft and Rockets. 20: 574-582. DOI: 10.2514/3.8589  0.432
1983 Nejad AS, Schetz JA. Effects of properties and location in the plume on droplet diameter for injection in a supersonic stream Aiaa Journal. 21: 956-961. DOI: 10.2514/3.8183  0.408
1983 Schetz JA, Jakubowski AK, Aoyagi K. Jet Trajectories and Surface Pressures Induced on a Body of Revolution with Various Dual Jet Configurations Journal of Aircraft. 20: 975-982. DOI: 10.2514/3.48201  0.488
1982 Hewitt P, Schetz JA. Atomization of Impinging Liquid Jets in a Supersonic Crossflow Aiaa Journal. 21: 178-179. DOI: 10.2514/3.8051  0.495
1982 Schetz JA, Figard RL. Numerical Solution of Flow Near the Rotor of a Wind Turbine Journal of Energy. 6: 65-70. DOI: 10.2514/3.62575  0.405
1980 Schetz JA, Kush EA, Joshi PB. Wave phenomena in liquid jet breakup in a supersonic crossflow Aiaa Journal. 18: 774-778. DOI: 10.2514/3.7687  0.371
1980 Figard RL, Schetz JA. Flowfield Near the Rotor of a 10 kW Horizontal-Axis Windmill Journal of Energy. 4: 64-69. DOI: 10.2514/3.62461  0.371
1980 Schetz JA, Cannon SC, Baranovsky S. Ignition of Liquid Fuel Jets in a Supersonic Air Stream Aiaa Journal. 18: 1101-1102. DOI: 10.2514/3.50859  0.464
1980 Baranovsky SI, Schetz JA. Effect of Injection Angle on Liquid Injection in Supersonic Flow Aiaa Journal. 18: 625-629. DOI: 10.2514/3.50798  0.428
1979 Figard RL, Schetz JA. Studies of the Aerodynamic Performance of a 10 kW Horizontal-Axis Windmill Journal of Energy. 3: 3-7. DOI: 10.2514/3.62403  0.431
1979 Swean TF, Schetz JA. Flow about a Propeller-Driven Body in Temperature-Stratified Fluid Aiaa Journal. 17: 863-869. DOI: 10.2514/3.61238  0.438
1977 Schetz JA, Nerney B. Turbulent boundary layer with injection and surface roughness Aiaa Journal. 15: 1288-1294. DOI: 10.2514/3.7415  0.439
1977 Schetz JA, Daffant EB. Aero/Hydrodynamic Forces and Moments on Self -Propelled Slender Bodies in Incompressible Flow Journal of Hydronautics. 11: 33-34. DOI: 10.2514/3.63199  0.336
1977 Schetz JA, Daffan EB, Jakubowski AK. Turbulent Wake Behind Slender Propeller-Driven Bodies At Angle Of Attack Aiaa Journal. 16: 6-7. DOI: 10.2514/3.60851  0.343
1977 Schetz JA, Padhye A. Penetration and Breakup of Liquids in Subsonic Airstreams Aiaa Journal. 15: 1385-1390. DOI: 10.2514/3.60805  0.358
1975 Schetz JA, Jakubowski AK. Experimental studies of the turbulent wake behind self-propelled slender bodies Aiaa Journal. 13: 1568-1575. DOI: 10.2514/3.7035  0.42
1975 Joshi PB, Schetz JA. Effect of Injector Shape on Penetration and Spread of Liquid Jets Aiaa Journal. 13: 1137-1138. DOI: 10.2514/3.60518  0.47
1975 Lorber AK, Schetz JA. Turbulent Mixing of Multiple Co-Axial Gaseous Fuel Jets in a Supersonic Airstream Aiaa Journal. 13: 973-974. DOI: 10.2514/3.60493  0.429
1975 Schetz JA, Overeem Jv. Skin Friction Reduction by Injection Through Combinations of Slots and Porous Sections Aiaa Journal. 13: 971-972. DOI: 10.2514/3.60492  0.457
1973 Schetz JA, Favin S, Ehrlich LW. Density Stratified, Viscous Flow past a Flat Plate Journal of Hydronautics. 7: 22-28. DOI: 10.2514/3.62925  0.396
1973 Kenworthy M, Schetz JA. Experimental Study of Slot Injection into a Supersonic Stream Aiaa Journal. 11: 585-586. DOI: 10.2514/3.50497  0.456
1973 Waltrup PJ, Schetz JA. Supersonic Turbulent Boundary Layer Subjected to Adverse Pressure Gradients Aiaa Journal. 11: 50-57. DOI: 10.2514/3.50435  0.438
1972 Campbell JF, Schetz JA. Flow properties of submerged heated effluents in a waterway. Aiaa Journal. 11: 223-230. DOI: 10.2514/3.50452  0.46
1970 Schetz J, Sherman A. Breakup of liquid sheets and jets in a supersonic gas stream Aiaa Journal. 9: 666-673. DOI: 10.2514/3.6246  0.361
1970 Schetz JA. Interaction Shock Shape for Transverse Injection in Supersonic Flow Journal of Spacecraft and Rockets. 7: 143-149. DOI: 10.2514/3.29889  0.414
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