Research Support
Grant: #2005U0001/Mod Investigators:Turner, Mark 05-15-2005 -09-30-2007 Department of the Air Force Engine Simulation Role:PI $585,504.00 Closed Level:Federal
Grant: #NCE Investigators:Turner, Mark 12-12-2003 -03-31-2005 National Aeronautics and Space Administration GE90 Turbine Simulation with Glenn-HT and APNASA Codes Role:PI $62,224.00 Closed Level:Federal
Grant: #OSP 04168/1 Investigators:Turner, Mark 03-31-2004 -12-31-2004 National Aeronautics and Space Administration Support/Consulting for Pulse Detonation Combustor-Turbine Simulations Role:PI $74,320.00 Closed Level:Federal
Grant: #S530-0002-34-C1/#2 Investigators:Turner, Mark 01-24-2005 -09-30-2007 Department of the Air Force Compressor Interaction Model Development Role:PI $71,576.00 Closed Level:Federal
Grant: #OSP 02117 Investigators:Turner, Mark 07-01-2001 -10-30-2001 National Aeronautics and Space Administration Turbofan Full Engine Simulation and Turbomachinery Design Role:PI $43,833.00 Closed Level:Federal
Grant: #OSP 02149/NAS3-01099 Investigators:Turner, Mark 11-15-2001 -10-30-2002 National Aeronautics and Space Administration NPSS GE90 Full Engine Simulation High Fidelity NPSS Combustor - High Pressure Turbine Interaction Role:PI $78,152.00 Closed Level:Federal
Grant: #OSP 02163/NAS3-99207 Investigators:Turner, Mark 03-15-2002 -09-30-2002 National Aeronautics and Space Administration 3D Turbomachinery Design System Development Role:PI $45,417.00 Closed Level:Federal
Grant: #OSP 03144 Investigators:Turner, Mark 01-01-2003 -11-30-2003 National Aeronautics and Space Administration CIAPP Automated Full Engine Simulation and Combustor-HPT Interaction Role:PI $126,251.00 Closed Level:Federal
Grant: #AV07-U-007 Investigators:Turner, Mark 10-31-2007 -10-31-2010 National Aeronautics and Space Administration Advanced Design Techniques for MDAO of Turbomachinery with Emphasis on Component Optimization for the Engine System Role:PI $241,179.00 Closed Level:Federal
Grant: #USAF-3446-26-SC-0001 Investigators:Orkwis, Paul; Turner, Mark 04-07-2008 -11-06-2008 Department of the Air Force Calculations for Experimental Aircraft Inlet Design Role:Collaborator $30,000.00 Closed Level:Federal
Grant: #TECH-09-022 Investigators:Abdallah, Shaaban; Cohen, Kelly; Hamed, Awatef; Jeng, San-Mou; Jog, Milind; Khosla, Prem; Lee, Jay; Qian, Dong; Schulz, Mark; Shanov, Vesselin; Singh, Raj; Steckl, Andrew; Turner, Mark; Vasudevan, Vijay; Walker, Bruce 08-18-2008 -08-17-2013 Ohio Department of Development Intelligent Propulsion and Power Systems and Their Life Management Role:Collaborator $27,492,308.00 Active Level:State of Ohio
Grant: #AFRL-000000441 Investigators:Orkwis, Paul; Turner, Mark 12-22-2008 -01-26-2010 Department of the Air Force Computational Fluid Dynamic Calculations to Support Shock Wave Boundary Layer Interaction Test Program in TGF Role:Collaborator $146,001.00 Closed Level:Federal
Grant: #Seed Grant Investigators:Turner, Mark 02-20-2009 -06-30-2010 National Aeronautics and Space Administration Promoting Science and Math Education Through Gas Turbine Restoration Role:PI $2,500.00 Closed Level:Federal
Grant: #PO 3580010880 Investigators:Turner, Mark 02-20-2009 -09-15-2010 Siemens Energy, Inc. Stator Rotor Unsteady CFD with Rim Cavity Using Numeca Fine/Turbo Role:PI $193,882.00 Closed Level:Industry
Grant: #PO#AFRL-0000001046 Investigators:Orkwis, Paul; Turner, Mark 10-19-2009 -11-30-2009 Department of the Air Force 2D CFD Simulations to Support Design of AFRL Glass Inlet Role:Collaborator $10,000.00 Closed Level:Federal
Grant: #AFRL-0000001289 Investigators:Orkwis, Paul; Turner, Mark 03-01-2010 -12-31-2011 Air Force Research Laboratory 3D CFD Simulations and Uncertainty Analysis to Support AFRL Mixed Compression Inlet Projects Role:Collaborator $271,493.00 Closed Level:Federal
Grant: #10-S590-0009-38-C1 / FA8650-08-D-2806 Investigators:Turner, Mark 10-01-2009 -11-22-2010 Department of the Air Force Small Turbine Engine Advanced Augmentor Research Role:PI $2,816.00 Closed Level:Federal
Grant: #2010 - 00730 Investigators:Turner, Mark 06-28-2010 -07-31-2011 Department of the Navy Vane Axial Flow CFD Support Role:PI $21,833.00 Closed Level:Federal
Grant: #3580016010 / DE-FC26-05NT42644 / Sub 038 Investigators:Turner, Mark 10-01-2010 -09-15-2012 Department of Energy Stator Rotor Unsteady CFD with Rim Cavity Using Numeca Fine/Turbo Role:PI $215,015.00 Active Level:Federal
Grant: #11-S590-0020-34-C3 Investigators:Turner, Mark 09-01-2011 -06-15-2012 Department of the Air Force Small Turbine Engine with Advanced Thrust Vectoring Role:PI $15,785.00 Closed Level:Federal
Grant: #AFRL-0000002588 Investigators:Orkwis, Paul; Turner, Mark 01-01-2012 -09-30-2012 Air Force Research Laboratory 3D CFD Simulations to Support AFRL Mixed Compression Inlet Projects Role:Collaborator $146,300.00 Closed Level:Federal
Grant: #12-S590-002-49-C6 \ FA8650-08-D-2806 Investigators:Turner, Mark 09-01-2012 -06-15-2013 Air Force Research Laboratory Exhaust Driven Fan Role:PI $14,498.00 Active Level:Federal
Grant: #2013-009-1 / W911QX-13-C-0133 Investigators:Turner, Mark 07-05-2013 -01-05-2014 Department of the Army Exploiting Unsteadiness for PDE Turbines Role:PI $29,000.00 Awarded Level:Federal
Grant: #13-S2604-04-C20 / FA8650-10-D-3037 Investigators:Orkwis, Paul; Turner, Mark 09-16-2013 -04-07-2014 Air Force Research Laboratory CFD Simulation and Modeling Support of AFRL SWBLI Experiments Role:Collaborator $50,000.00 Awarded Level:Federal
Grant: #13-S590-0020-63-C5 Investigators:Turner, Mark 09-01-2013 -06-15-2014 Air Force Research Laboratory Power Takeoff Turbine for the 2013/2014 Aerospace Propulsion Outreach Program (APOP) Role:PI $12,000.00 Awarded Level:Federal
Grant: #PO 200-1J--1BH32382 (RFQ 535-BLANKET) Investigators:Jeng, San-Mou; Jog, Milind; Lee, Jongguen; Tambe, Samir; Turner, Mark 11-26-2013 -12-31-2016 General Electric - GE Transportation - Aircraft Division Blanket PO for FY2014, FY 2015, and FY2016 Role:Collaborator $900,000.00 Awarded Level:Industry
Grant: #15-7900-0005-03-C$ / AF FA8650-14-D-2411 Investigators:Turner, Mark 10-21-2014 -06-15-2015 Air Force Research Laboratory 2014-2015 Aerospace Propulsion Outreach Program (APOP): Power Takeoff Turbine Role:PI $10,000.00 Awarded Level:Federal
Grant: #15-7900-0006-10-C7 / FA8650-14-D-2411 Investigators:Turner, Mark 09-21-2015 -07-31-2016 Air Force Research Laboratory 2015-2016 APOP - Cooled/Hi-Temperature Turbine Role:PI $14,875.00 Awarded Level:Federal
Grant: #VPL-15-006/NNC12BA01B Investigators:Turner, Mark 10-01-2015 -02-29-2016 National Aeronautics and Space Administration Computational Investigation of Turbine Aerodynamics and Heat Transfer - Purge Flow Vane Design Role:PI $4,749.00 Awarded Level:Federal
Grant: #VPL-16-164/NNC12BA01B Investigators:Turner, Mark 05-24-2016 -05-31-2017 National Aeronautics and Space Administration Unsteady Turbine Simulation Capability Role:PI $39,000.00 Active Level:Federal
Grant: #USAF CRADA FY-DAY-LAB# 16-266-RQ-01 Investigators:Orkwis, Paul; Turner, Mark 06-16-2016 -06-15-2021 Air Force Research Laboratory Development of Algorithms for High Order Accurate CFD Simulations Role:Collaborator $.00 Active Level:Federal
Grant: #16-7900-0008-15-C7 / FA8650-14-D-2411 Investigators:Turner, Mark 09-01-2016 -05-31-2017 Air Force Research Laboratory Propulsor and Cycle Development for APOP Role:PI $4,027.00 Active Level:Federal
Grant: #AFRL EPA# 17-EPA-RQ-06 Investigators:Turner, Mark 12-01-2016 -11-30-2021 Air Force Research Laboratory Education Partnership Agreement between Aerospace Systems Directorate (AFRL) and University of Cincinnati Role:PI $.00 Active Level:Federal
Grant: #VPL-17-066 / NNC12BA01B GESS3 Investigators:Turner, Mark 04-01-2017 -11-30-2017 National Aeronautics and Space Administration Preliminary Robust Fan and Inlet Designs for BLI Role:PI $122,798.00 Active Level:Federal
Grant: #DAGSI RQ22-UC-17-2 sub ODHE Investigators:Turner, Mark 05-01-2017 -04-30-2018 Ohio Department of Higher Education Thrust to Weight Ratio Improvement if Netcat P400 Role:PI $52,260.00 Active Level:State of Ohio
Grant: #STTR PO# 2017-00597 Investigators:Turner, Mark 07-01-2017 -10-31-2017 Department of the Navy Reduced Cavitation, High Efficiency Outboard Propulsors for Small Planing Craft Role:PI $50,489.00 Active Level:Federal
Grant: #17-7900-0008-32-C7 / FA8650-14-D-2411 TO FA8650-16-F-2639-0008 Investigators:Turner, Mark 08-01-2017 -07-31-2018 Department of the Air Force Distributed Propulsive Cycle for the 2017-2018 APOP Role:PI $2,740.00 Active Level:Federal
Grant: #OSU 60057639 sub WSARC-1077-200 sub ODHE Investigators:Munday, David; Turner, Mark 09-19-2016 -01-31-2019 Ohio Department of Higher Education Advanced Turbine Cooling Role:PI $267,268.00 Active Level:State of Ohio
Grant: #IGTI Student Scholarship (Kumar) Investigators:Kumar, Sandeep; Turner, Mark 10-12-2018 -10-11-2019 American Society of Mechanical Engineers Gas Turbine or Turbomachinery Industry Fellowship Role:Collaborator $2,000.00 Awarded Level:Private Non-Profit
Grant: #18-7900-0008-38-C7 / FA8650-14-D-2411 TO FA8650-16-F-2639 (0008) Investigators:Abdallah, Shaaban; Turner, Mark 08-01-2018 -06-30-2019 Department of the Air Force Request for Proposal (RFP): 2018/2019 Aerospace Propulsion Outreach Program (APOP) Role:PI $5,090.00 Awarded Level:Federal
Grant: #PO 2018-0788 / N68335-18-C-0712 Investigators:Turner, Mark 08-31-2018 -02-08-2019 Department of the Navy New Integrated Total Design of Unmanned Underwater Vehicles (UUVs) Propulsion System Architecture for Higher Efficiency and Low Noise Role:PI $52,399.00 Awarded Level:Federal
Grant: #142411-16F2639-19-48-C7 / FA8650-14-D-2411/FA8650-16-F-2639 (TO0008) Investigators:Turner, Mark 08-01-2019 -06-30-2020 Department of the Air Force 2019/2020 Aerospace Propulsion Outreach Program (APOP) Role:PI $2,545.00 Awarded Level:Federal
Grant: #R40316 Investigators:Turner, Mark 01-01-2020 -04-30-2020 UC's Faculty Bridge Program stipend support for PhD student, Mayank Sharma (DOE project) Role:PI $5,000.00 Active Level:Internal UC
Grant: #2019-2107 / N68335-20-C-0043 Investigators:Turner, Mark 11-01-2019 -10-31-2022 Department of the Navy New Integrated Total Design of Unmanned Underwater Vehicles (UUVs) Propulsion System Architecture for Higher Efficiency and Low Noise Role:PI $149,999.00 Awarded Level:Federal
Grant: #DE-EE000887 Investigators:Turner, Mark 04-01-2020 -03-31-2023 Department of Energy Carbon Dioxide Compressor Design for Thermal Storage Application Role:PI $222,379.00 Active Level:Federal
Grant: #Cornerstone UC PO 2019-2058_W56HZV-19-C-0102 Investigators:Turner, Mark 09-30-2019 -03-31-2020 Department of the Army Electric Coolant Pump for High-Temperature Power Generation Cooling Applications Role:PI $15,500.00 Active Level:Federal
Grant: #142411-16F2639-20-53-C1 / FA8650-14-D-2411 (TO 0008) Investigators:Turner, Mark 08-31-2020 -03-26-2021 Department of the Air Force 2020/2021 Aerospace Propulsion Outreach Program (APOP) Role:PI $7,371.00 Active Level:Federal
Grant: #OSGC (Wells) Scholarship Investigators:Turner, Mark; Wells, Kaden 11-01-2020 -10-31-2021 Ohio Department of Higher Education Wells OSGC Scholarship Role:PI $3,500.00 Awarded Level:State of Ohio
Grant: #STEM ck #3156 (M. Bill) Investigators:Turner, Mark 11-01-2020 -10-31-2021 NASA Headquarters DOE AND UUV Propulsor _M. Bill Role:PI $7,000.00 Awarded Level:Federal
Grant: #PO 2020-2358 / FA864921P0033 Investigators:Turner, Mark 12-22-2020 -05-21-2021 Air Force Office of Scientific Research Propulsion Design in Support of AFWERX Concepts Role:PI 50000.00 Active Level:Federal
Publications
Peer Reviewed Publications
Mcclanahan D.R.;Liu G.R.;Turner M.G.;Anantharaman D. (09-01-2019). Topology Optimization of the Interior Structure of Blades with an Outer Surface Determined Through A. International Journal of Computational Methods, 16 (6) More Information
Kalagotla D.;Orkwis P.;Turner M. (01-01-2018). Modeling particle drag in accelerating flows with implications for SBLI in PIV-a numerical analysis. 2018 Fluid Dynamics ConferenceMore Information
Wukie N.;Turner M.;Orkwis P. (01-01-2018). A neumann pressure outlet boundary condition for compressible flows. 2018 Fluid Dynamics ConferenceMore Information
Sharma M.;Wukie N.A.;Ugolotti M.;Turner M.G. (01-01-2018). Unsteady turbomachinery simulations using harmonic balance on a discontinuous galerkin discretizatio. Proceedings of the ASME Turbo Expo, 2C-2018More Information
Kumar S.;Turner M.G.;Siddappaji K.;Celestina M. (01-01-2018). Aerodynamic design system for non-axisymmetric boundary layer ingestion fans. Proceedings of the ASME Turbo Expo, 2C-2018More Information
Ugolotti M.;Wukie N.;Turner M.;Orkwis P.D. (01-01-2018). Discrete-adjoint solver tests and consistency analysis for discontinuous galerkin discretization. 2018 Fluid Dynamics ConferenceMore Information
Mahmood S.;Turner M. (01-01-2017). Modeling capability for cavity flows in an axial compressor. Proceedings of the ASME Turbo Expo, 2B-2017More Information
Woeste J.;Turner M.;Saxer N. (01-01-2017). A hydrofoil configuration for wind powered energy ship applications. American Society of Mechanical Engineers, Fluids Engineering Division (Publication) FEDSM, 1B-2017More Information
Balasubramanian K.;Turner M.G.;Siddappaji K. (01-01-2017). Novel curvature-based airfoil parameterization for wind turbine application and optimization. Proceedings of the ASME Turbo Expo, 9More Information
Balachandar S.; Ouwerkerk J.; Owen M.; Sharma M.; Turner M.; Ugolotti M.; Williams Z. (01-01-2017). Cooling system for 0.1 kN thrust micro-engines: Concept design using additive manufacturing. 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017
Wukie N.;Orkwis P.;Turner M. (01-01-2016). An implicit, discontinuous Galerkin Chimera solver using automatic differentiation. 54th AIAA Aerospace Sciences Meeting, 0
Mishra S.;Abdallah S.;Turner M. (01-01-2016). Flow characteristics of a novel centrifugal compressor design. Proceedings of the ASME Turbo Expo, 2D-2016More Information
Mahmood S.;Turner M.;Siddappaji K. (01-01-2016). Flow characteristics of an optimized axial compressor rotor using smooth design parameters. Proceedings of the ASME Turbo Expo, 2C-2016More Information
Schroder A.;Turner M.;Roberts R. (01-01-2016). Combined cycle engine cascades achieving high efficiency. Proceedings of the ASME Turbo Expo, 3More Information
Orkwis P.; Turner M.; Wukie N. (01-01-2016). A fully-implicit, Giles-type nonreflecting boundary condition in a DG-Chimera turbomachinery solver. 46th AIAA Fluid Dynamics Conference
Chen H.;Turner M.;Siddappaji K.;Mahmood S. (01-01-2016). Vorticity dynamics based flow diagnosis for a 1.5-stage high pressure compressor with an optimized t. Proceedings of the ASME Turbo Expo, 2A-2016More Information
Turner M.;Roberts R.;Rumpfkeil M.;Vankuren J.;Bons J.;Smith T.;Ausserer J.;Litke P. (01-01-2016). Thrust vectoring design project at six universities. International Journal of Engineering Education, 32 (1) , 252-271
Holden J.R.;Caley T.M.;Heberling B.;Cantor C.;Wesseling E.;Hamed A.A.;Turner M.G.;Litke P.J.;Grannan N. (01-01-2016). Novel design and fabrication of JetCat P90 diffuser using parametric design and optimization tools. 54th AIAA Aerospace Sciences Meeting
Galbraith M.;Benek J.;Orkwis P.;Turner M. (09-02-2015). A discontinuous Galerkin scheme for Chimera overset viscous meshes on curved geometries. Computers and Fluids, 119, 176-196More Information
Siddappaji K.;Turner M. (01-01-2015). Revolutionary geometries of mobile hydrokinetic turbines for wind energy applications. Proceedings of the ASME Turbo Expo, 9More Information
Holden J.;Caley T.;Turner M. (01-01-2015). Maple seed performance as a wind turbine. 53rd AIAA Aerospace Sciences MeetingMore Information
Wukie N.A.;Orkwis P.D.;Turner M.G.;Duncan S. (01-01-2015). Simulations and models for aspiration in a supersonic flow using OVERFLOW. AIAA Journal, 53 (7) , 2052-2056More Information
Gannon A.;Hobson G.;Turner M.;Sanz W. (01-01-2015). Performance of a splittered transonic rotor with several tip clearances. Proceedings of the ASME Turbo Expo, 2AMore Information
Friedlander D.J.;Georgiadis N.J.;Turner M.G.;Orkwis P.D. (01-01-2015). Numerical simulations of the University of Michigan shock boundary-layer interaction experiments. AIAA Journal, 53 (5) , 1134-1145More Information
Schrock C.R.;Beneky J.A.;Knapke R.;Turner M.;Galbraith M.C. (01-01-2015). Evaluation of a discontinuous galerkin implementation of RANS and spalart allmaras turbulence model. 53rd AIAA Aerospace Sciences MeetingMore Information
Turner M.;Nemnem A.;Gannon A.;Hobson G.;Sanz W. (01-01-2015). Measured heat transfer in a transonic fan rig at casing with implications on performance. Proceedings of the ASME Turbo Expo, 2AMore Information
Galbraith M.;Benek J.;Orkwis P.;Turner M. (07-02-2014). A Discontinuous Galerkin Chimera scheme. Computers and Fluids, 98, 27-53More Information
Nemnem A.;Turner M.;Siddappaji K.;Galbraith M. (01-01-2014). A smooth curvature-defined meanline section option for a general turbomachinery geometry generator. Proceedings of the ASME Turbo Expo, 2BMore Information
Knapke R.D.;Turner M.G.;Galbraith M.;Orkwis P. (01-01-2014). A high-order implict harmonic balance method for turbomachinery applications. 15th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2014
Knapke R.;Turner M. (12-17-2013). Unsteady simulations of a counter-rotating aspirated compressor. Proceedings of the ASME Turbo Expo, 6 AMore Information
Bruna D.;Turner M. (12-17-2013). A rothalpy analysis for the isothermal boundary condition at casing applied to the rotor 37 transoni. Proceedings of the ASME Turbo Expo, 6 BMore Information
Rumpfkeil M.;Turner M.;Van Kuren J.;Roberts R.;Bons J.;Smith T.;Ausserer J. (12-17-2013). Thrust vectoring design project at six universities (PART II): Impact on student learning and lesson. Proceedings of the ASME Turbo Expo, 4More Information
Turner M.;Rumpfkeil M.;VanKuren J.;Roberts R.;Bons J.;Smith T.;Ausserer J.;Litke P. (12-17-2013). Thrust vectoring design project at six universities (PART I): Project description and final designs. Proceedings of the ASME Turbo Expo, 4More Information
Friedlander D.; Georgiadis N.; Orkwis P.; Turner M. (08-19-2013). Computational fluid dynamic (CFD) analyses of the university of Michigan's shock boundary-layer inte. 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013
Galbraith M.; Knapke R.; Orkwis P.; Turner M. (08-19-2013). An implicit Harmonic balance method with a Discontinuous Galerkin spatial scheme. 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013
Orkwis P.D.;Turner M.G.;Apyan A.;Flenar K.;Duncan S.;Wukie N.;Benek J. (08-19-2013). Modeling and simulation of bleed holes in the presence of shock wave/boundary layer interaction. 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013
Knapke R.;Turner M. (03-07-2013). Detailed unsteady simulation of a counterrotating aspirated compressor with a focus on the aspiratio. International Journal of Rotating Machinery, 2013More Information
Siddappaji K.;Turner M.G.;Merchant A. (12-01-2012). General capability of parametric 3D blade design tool for turbomachinery. Proceedings of the ASME Turbo Expo, 8 (PARTS A, B, AND C) , 2331-2344More Information
Wukie N.A.;Orkwis P.D.;Turner M.G.;Duncan S. (12-01-2012). Comparison of simulations and models for aspiration in a supersonic flow using OVERFLOW. 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace ExpositionMore Information
Apyan A.;Orkwis P.;Turner M.;Duncan S.;Benek J.;Tinnaple J. (12-01-2012). Mixed compression inlet simulations with aspiration. 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace ExpositionMore Information
Bruna D.;Turner M. (06-25-2012). Isothermal boundary condition at casing applied to the rotor 37 transonic axial flow compressor. Journal of Turbomachinery, 135 (3) More Information
Bruna D.;Cravero C.;Turner M.;Merchant A. (05-08-2012). An Educational Software Suite for Teaching Design Strategies for Multistage Axial Flow Compressors. Journal of Turbomachinery, 134 (5) More Information
DeBonis J.R.;Oberkampf W.L.;Wolf R.T.;Orkwis P.D.;Turner M.G.;Babinsky H.;Benek J.A. (04-01-2012). Assessment of computational fluid dynamics and experimental data for shock boundary-layer interactio. AIAA Journal, 50 (4) , 891-903More Information
Park K.;Turner M.;Siddappaji K.;Dey S.;Merchant A. (12-01-2011). Optimization of a 3-stage booster part 1: The axisymmetric multi-disciplinary optimization approach . Proceedings of the ASME Turbo Expo, 7 (PARTS A, B, AND C) , 1413-1422More Information
Siddappaji K.;Turner M.;Dey S.;Park K.;Merchant A. (12-01-2011). Optimization of a 3-stage booster-part 2: The parametric 3D blade geometry modeling tool. Proceedings of the ASME Turbo Expo, 7 (PARTS A, B, AND C) , 1431-1443More Information
Soliman S.;Abdallah S.;Gutmark E.;Turner M. (04-10-2011). Numerical simulation of microparticles penetration and gas dynamics in an axi-symmetric supersonic n. Powder Technology, 208 (3) , 676-683More Information
Turner M.;Merchant A.;Bruna D. (01-01-2011). A turbomachinery design tool for teaching design concepts for axial-flow fans, compressors, and turb. Journal of Turbomachinery, 133 (3) More Information
Turner M.G.;Gorrell S.E.;Car D. (01-01-2011). Radial migration of shed vortices in a transonic rotor following a wake generator: A comparison betw. Journal of Turbomachinery, 133 (3) More Information
Turner M. (12-13-2010). Lessons learned from the GE90 3D full engine simulations. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
Galbraith D.;Galbraith M.;Turner M.;Orkwis P.;Apyan A. (12-13-2010). Preliminary numerical investigation of a mach 3 inlet configuration with and without aspiration and . 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
Galbraith D.S.;Turner M.G.;Orkwis P.D.;Galbraith M.C.;Driscoll J.F.;Eagle E. (12-02-2010). Design of a glass supersonic wind tunnel experiment for mixed compression inlet investigations. 40th AIAA Fluid Dynamics Conference
Gutzwiller D.;Turner M. (12-01-2010). Low fidelity turbomachinery disk design studies. Proceedings of the ASME Turbo Expo, 6 (PARTS A AND B) , 1309-1324More Information
Turner M.G.;Park K.;Siddappaji K.;Dey S.;Gutzwiller D.P.;Merchant A.;Bruna D. (12-01-2010). Framework for multidisciplinary optimization of turbomachinery. Proceedings of the ASME Turbo Expo, 7 (PARTS A, B, AND C) , 623-631More Information
Gutzwiller D.;Turner M. (01-01-2010). Rapid low fidelity turbomachinery disk optimization. Advances in Engineering Software, 41 (5) , 779-791More Information
List M.;Gorrell S.;Turner M. (01-01-2010). Investigation of Loss Generation in an Embedded Transonic Fan Stage at Several Gaps Using High-Fidel. Journal of Turbomachinery, 132 (1) More Information
Guidotti E.;Turner M.G. (12-01-2009). Analysis of the unsteady flow in an aspirated counter-rotating compressor using the nonlinear harmon. Proceedings of the ASME Turbo Expo, 7 (PART A) , 685-698More Information
Gutzwiller D.;Turner M.;Downing M. (12-01-2009). Educational software for blade and disk design. Proceedings of the ASME Turbo Expo, 1, 827-838More Information
Claus R.;Lavelle T.;Townsend S.;Turner M. (12-01-2009). Coupled component, full engine simulation of a gas turbine engine. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Szabo I.;Turner M. (12-01-2008). An entropy based evaluation of efficiency of a transonic compressor rotor with water injection. Proceedings of the ASME Turbo Expo, 6 (PART A) , 167-179More Information
List M.;Gorrell S.;Turner M. (12-01-2008). Investigation of loss generation in an embedded transonic fan stage at several gaps using high fidel. Proceedings of the ASME Turbo Expo, 6 (PART C) , 2599-2609More Information
Claus R.;Lavelle T.;Townsend S.;Turner M. (12-01-2008). Coupled high-fidelity engine system simulation. ICAS Secretariat - 26th Congress of International Council of the Aeronautical Sciences 2008, ICAS 2008, 1, 4140-4149
Claus R.;Lavelle T.;Townsend S.;Turner M. (12-01-2008). Challenges in the development of a multi-fidelity, coupled component simulation of complex systems. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Knapke R.;Turner M.;List M.;Galbraith D.;Beach T.;Merchant A. (12-01-2008). Time accurate simulations of a counter-rotating aspirated compressor. Proceedings of the ASME Turbo Expo, 6 (PART A) , 481-496More Information
Claus R.W.;Lavelle T.;Townsend S.;Turner M.;Reed J. (12-11-2007). Variable fidelity analysis of complete engine systems. Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 1, 394-402
Turner M.G.;Merchant A.;Bruna D. (12-10-2007). Applications of a turbomachinery design tool for compressors and turbines. Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2, 1491-1501
List M.G.;Gorrell S.E.;Turner M.G.;Nimersheim J.A. (12-10-2007). High fidelity modeling of blade row interaction in a transonic compressor. Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 1, 424-437
List M.G.;Turner M.G.;Galbraith D.S.;Nimersheim J.A.;Galbraith M.C. (12-10-2007). High-resolution, parallel visualization of turbomachinery flowfields. Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 1, 403-413
Mavriplis D.J.;Darmofal D.;Keyes D.;Turner M. (11-07-2007). Petaflops opportunities for the NASA fundamental aeronautics program. Collection of Technical Papers - 18th AIAA Computational Fluid Dynamics Conference, 1, 775-810
Bruna D.;Cravero C.;Turner M.;Merchant A. (09-24-2007). An educational software suite for teaching design strategies for multistage axial flow compressors. Proceedings of the ASME Turbo Expo, 3, 465-474More Information
Szabo I.;Turner M.G. (07-03-2007). A numerical study of water injection on transonic compressor rotor performance. Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting, 1, 97-110
Kamp M.A.;Nimersheim J.;Beach T.;Turner M.G. (07-02-2007). A turbomachinery gridding system. Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting, 1, 111-123
Turner M.G.;Gorrell S.E.;Car D. (12-01-2006). A model of compressor blade row interaction with shock induced vortex shedding. Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference, 2, 1410-1422
Claus R.W.;Townsend S.;Lavelle T.;Naiman C.;Turner M. (12-01-2006). A case study of high fidelity engine system simulation. Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference, 8, 6188-6197
Bruna D.;Cravero C.;Turner M. (11-15-2006). The development of an aerodynamic performance prediction tool for modern axial flow compressor profi. Proceedings of the ASME Turbo Expo, 6 PART A, 113-122More Information
Turner M.;Merchant A.;Bruna D. (11-14-2006). A turbomachinery design tool for teaching design concepts for axial-flow fans, compressors, and turb. Proceedings of the ASME Turbo Expo, 1, 937-952More Information
Lukovic B.;Orkwis P.D.;Turner M.G.;Sekar B. (07-01-2006). Neural network modeling of deterministic unsteadiness source terms. AIAA Journal, 44 (7) , 1609-1616More Information
Reed J.;Turner M. (11-24-2005). An entropy loss approach for a meanline bladerow model with coupling to test data and 3D CFD results. Proceedings of the ASME Turbo Expo, 6 PART B, 1127-1136More Information
Turner M.G.;Gorrell S.E.;Car D. (11-24-2005). Radial migration of shed vortices in a transonic rotor following a wake generator: A comparison betw. Proceedings of the ASME Turbo Expo, 6 PART B, 1195-1209More Information
Kukreti A.;Islam S.;Oerther D.;Davis K.;Turner M.;Maltbie C.;Fowler T. (01-01-2005). Investigating student interest in post-secondary STEM education. ASEE Annual Conference and Exposition, Conference Proceedings, 9021-9036
Shabbir A.;Turner M.G. (12-22-2004). A wall function for calculating the skin friction with surface roughness. Proceedings of the ASME Turbo Expo 2004, 5 B, 1661-1671
Turner M.G.;Ryder R.;Reed J.A.;Veres J.P. (12-22-2004). Multi-fidelity simulation of a turbofan engine with results zoomed into mini-maps for a Zero-D cycle. Proceedings of the ASME Turbo Expo 2004, 2, 219-230
List M.;Turner M.;Chen J.;Remotigue M.;Veres J. (07-01-2004). Unsteady cooled turbine solutions using a PC-Linux analysis system. AIAA Paper, 28-39
Turner M.;Norris A.;Veres J. (12-01-2003). High fidelity 3D simulation of the GE90. 33rd AIAA Fluid Dynamics Conference and Exhibit
Filz C.;Lee D.;Orkwis P.;Turner M. (12-01-2003). Modeling of two dimensional directed synthetic jets using neural network-based deterministic source . 33rd AIAA Fluid Dynamics Conference and Exhibit
Lee D.;Orkwist P.;Turner M.;Pes M.;Filz C.;Caldwell N. (12-01-2003). Numerical analysis of two dimensional directed synthetic jets in cross flow at low mach number. 41st Aerospace Sciences Meeting and Exhibit
Lukovic B.;Orkwis P.;Turner M. (12-01-2002). Modeling unsteady cavity flows with translating walls. 32nd AIAA Fluid Dynamics Conference and Exhibit
Lukovic B.; Orkwis P.; Sekar B.; Turner M. (12-01-2002). Effect of cavity L/D variations on neural network-based deterministic unsteadiness source terms. 40th AIAA Aerospace Sciences Meeting and Exhibit
Turner M.;Ryder R.;Norris A.;Celestina M.;Moder J.;Liu N.;Adamczyk J.;Veres J. (12-01-2002). High fidelity 3D turbofan engine simulation with emphasis on turbomachinery-combustor coupling. 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Orkwis P.D.;Turner M.G.;Barter J.W. (01-01-2002). Linear deterministic source terms for hot streak simulations. Journal of Propulsion and Power, 18 (2) , 383-389More Information
Orkwis P.;Turner M.;Barter J. (01-01-2000). Linear deterministic source terms for hot streak simulations. Proceedings of the ASME Turbo Expo, 1More Information
Kirtley K.;Turner M.;Saeidi S. (01-01-1999). An average passage closure model for general meshes. Proceedings of the ASME Turbo Expo, 1More Information
Turner M.;Vitt P.;Topp D.;Saeidi S.;Hunter S.;Dailey L.;Beach T. (01-01-1999). Multistage simulations of the GE90 turbine. Proceedings of the ASME Turbo Expo, 1More Information
Turner M. (01-01-1996). Multistage turbine simulations with vortex-blade interaction. Journal of Turbomachinery, 118 (4) , 643-653More Information
Chiang H.;Turner M. (01-01-1996). Compressor blade forced response due to downstream vane-strut potential interaction. Journal of Turbomachinery, 118 (1) , 134-142More Information
Turner M. (01-01-1995). Multistage turbine simulations with vortex-blade interaction. Proceedings of the ASME Turbo Expo, 1More Information
Turner M. (01-01-1995). Multistage turbine simulations with vortex-blade interaction. American Society of Mechanical Engineers (Paper)
Jennions I.;Turner M. (01-01-1993). Three-dimensional navier-stokes computations of transonic fan flow using an explicit flow solver and. Journal of Turbomachinery, 115 (2) , 261-272More Information
Turner M.;Jennions I. (01-01-1993). An investigation of turbulence modeling in transonic fans including a novel implementation of an imp. Journal of Turbomachinery, 115 (2) , 249-260More Information
Chiang H.;Turner M. (01-01-1993). Compressor blade forced response due to downstream vane-strut potential interaction. ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition, GT 1993, 3BMore Information
Chiang H.;Turner M. (01-01-1993). Compressor blade forced response due to downstream vane-strut potential interaction. American Society of Mechanical Engineers (Paper), 1-12
Turner M.;Liang T.;Beauchamp P.;Jennions I. (01-01-1993). The use of orthogonal grids in turbine CFD computations. ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition, GT 1993, 1More Information
Turner M.;Liang T.;Beachamp P.;Jennions I. (01-01-1993). Use of orthogonal grids in turbine CFD computations. American Society of Mechanical Engineers (Paper), 1-16
Jennions I.;Turner M. (01-01-1992). Three-dimensional Navier-Stokes computations of transonic fan flow using an explicit flow solver and. ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition, GT 1992, 1More Information
Turner M.;Jennions I. (01-01-1992). An investigation of turbulence modelling in transonic fans including a novel implementation of an im. ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition, GT 1992, 1More Information