Mark Turner

Mark G. Turner

Professor

Baldwin Hall

745C

CEAS - Aerospace Eng - 0070

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

Publications

Peer Reviewed Publications

Anantharaman D.; Liu G.; Mcclanahan D.; Turner M. (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 ),

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 Conference, ,

Orkwis P.; Turner M.; Wukie N. (01-01-2018. )A neumann pressure outlet boundary condition for compressible flows.2018 Fluid Dynamics Conference, ,

Sharma M.; Turner M.; Ugolotti M.; Wukie N. (01-01-2018. )Unsteady turbomachinery simulations using harmonic balance on a discontinuous galerkin discretizatio.Proceedings of the ASME Turbo Expo, ,2C-2018 ,

Celestina M.; Kumar S.; Siddappaji K.; Turner M. (01-01-2018. )Aerodynamic design system for non-axisymmetric boundary layer ingestion fans.Proceedings of the ASME Turbo Expo, ,2C-2018 ,

Orkwis P.; Turner M.; Ugolotti M.; Wukie N. (01-01-2018. )Discrete-adjoint solver tests and consistency analysis for discontinuous galerkin discretization.2018 Fluid Dynamics Conference, ,

Mahmood S.; Turner M. (01-01-2017. )Modeling capability for cavity flows in an axial compressor.Proceedings of the ASME Turbo Expo, ,2B-2017 ,

Saxer N.; Turner M.; Woeste J. (01-01-2017. )A hydrofoil configuration for wind powered energy ship applications.American Society of Mechanical Engineers, Fluids Engineering Division (Publication) FEDSM, ,1B-2017 ,

Balasubramanian K.; Siddappaji K.; Turner M. (01-01-2017. )Novel curvature-based airfoil parameterization for wind turbine application and optimization.Proceedings of the ASME Turbo Expo, ,9 ,

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, ,

Orkwis P.; Turner M.; Wukie N. (01-01-2016. )An implicit, discontinuous Galerkin Chimera solver using automatic differentiation .54th AIAA Aerospace Sciences Meeting, ,0 ,

Abdallah S.; Mishra S.; Turner M. (01-01-2016. )Flow characteristics of a novel centrifugal compressor design.Proceedings of the ASME Turbo Expo, ,2D-2016 ,

Mahmood S.; Siddappaji K.; Turner M. (01-01-2016. )Flow characteristics of an optimized axial compressor rotor using smooth design parameters.Proceedings of the ASME Turbo Expo, ,2C-2016 ,

Roberts R.; Schroder A.; Turner M. (01-01-2016. )Combined cycle engine cascades achieving high efficiency.Proceedings of the ASME Turbo Expo, ,3 ,

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.; Mahmood S.; Siddappaji K.; Turner M. (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-2016 ,

Ausserer J.; Bons J.; Litke P.; Roberts R.; Rumpfkeil M.; Smith T.; Turner M.; Vankuren J. (01-01-2016. )Thrust vectoring design project at six universities .International Journal of Engineering Education, ,32 (1 ),252-271

Caley T.; Cantor C.; Grannan N.; Hamed A.; Heberling B.; Holden J.; Litke P.; Turner M.; Wesseling E. (01-01-2016. )Novel design and fabrication of JetCat P90 diffuser using parametric design and optimization tools .54th AIAA Aerospace Sciences Meeting, ,

Benek J.; Galbraith M.; Orkwis P.; Turner M. (09-02-2015. )A discontinuous Galerkin scheme for Chimera overset viscous meshes on curved geometries.Computers and Fluids, ,119 ,176-196

Siddappaji K.; Turner M. (01-01-2015. )Revolutionary geometries of mobile hydrokinetic turbines for wind energy applications.Proceedings of the ASME Turbo Expo, ,9 ,

Caley T.; Holden J.; Turner M. (01-01-2015. )Maple seed performance as a wind turbine.53rd AIAA Aerospace Sciences Meeting, ,

Duncan S.; Orkwis P.; Turner M.; Wukie N. (01-01-2015. )Simulations and models for aspiration in a supersonic flow using OVERFLOW.AIAA Journal, ,53 (7 ),2052-2056

Gannon A.; Hobson G.; Sanz W.; Turner M. (01-01-2015. )Performance of a splittered transonic rotor with several tip clearances.Proceedings of the ASME Turbo Expo, ,2A ,

Friedlander D.; Georgiadis N.; Orkwis P.; Turner M. (01-01-2015. )Numerical simulations of the University of Michigan shock boundary-layer interaction experiments.AIAA Journal, ,53 (5 ),1134-1145

Beneky J.; Galbraith M.; Knapke R.; Schrock C.; Turner M. (01-01-2015. )Evaluation of a discontinuous galerkin implementation of RANS and spalart allmaras turbulence model.53rd AIAA Aerospace Sciences Meeting, ,

Gannon A.; Hobson G.; Nemnem A.; Sanz W.; Turner M. (01-01-2015. )Measured heat transfer in a transonic fan rig at casing with implications on performance.Proceedings of the ASME Turbo Expo, ,2A ,

Benek J.; Galbraith M.; Orkwis P.; Turner M. (07-02-2014. )A Discontinuous Galerkin Chimera scheme.Computers and Fluids, ,98 ,27-53

Galbraith M.; Nemnem A.; Siddappaji K.; Turner M. (01-01-2014. )A smooth curvature-defined meanline section option for a general turbomachinery geometry generator.Proceedings of the ASME Turbo Expo, ,2B ,

Galbraith M.; Knapke R.; Orkwis P.; Turner M. (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 A ,

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 B ,

Ausserer J.; Bons J.; Roberts R.; Rumpfkeil M.; Smith T.; Turner M.; Van Kuren 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, ,4 ,

Ausserer J.; Bons J.; Litke P.; Roberts R.; Rumpfkeil M.; Smith T.; Turner M.; VanKuren J. (12-17-2013. )Thrust vectoring design project at six universities (PART I): Project description and final designs.Proceedings of the ASME Turbo Expo, ,4 ,

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, ,

Apyan A.; Benek J.; Duncan S.; Flenar K.; Orkwis P.; Turner M.; Wukie N. (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, ,2013 ,

Merchant A.; Siddappaji K.; Turner M. (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 ),2331-2344

Duncan S.; Orkwis P.; Turner M.; Wukie N. (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 Exposition, ,

Apyan A.; Benek J.; Duncan S.; Orkwis P.; Tinnaple J.; Turner M. (12-01-2012. )Mixed compression inlet simulations with aspiration.50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, ,

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 ),

Bruna D.; Cravero C.; Merchant A.; Turner M. (05-08-2012. )An Educational Software Suite for Teaching Design Strategies for Multistage Axial Flow Compressors.Journal of Turbomachinery, ,134 (5 ),

Babinsky H.; Benek J.; DeBonis J.; Oberkampf W.; Orkwis P.; Turner M.; Wolf R. (04-01-2012. )Assessment of computational fluid dynamics and experimental data for shock boundary-layer interactio.AIAA Journal, ,50 (4 ),891-903

Dey S.; Merchant A.; Park K.; Siddappaji K.; Turner M. (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 ),1413-1422

Dey S.; Merchant A.; Park K.; Siddappaji K.; Turner M. (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 ),1431-1443

Abdallah S.; Gutmark E.; Soliman S.; Turner M. (04-10-2011. )Numerical simulation of microparticles penetration and gas dynamics in an axi-symmetric supersonic n.Powder Technology, ,208 (3 ),676-683

Bruna D.; Merchant A.; Turner M. (01-01-2011. )A turbomachinery design tool for teaching design concepts for axial-flow fans, compressors, and turb.Journal of Turbomachinery, ,133 (3 ),

Car D.; Gorrell S.; Turner M. (01-01-2011. )Radial migration of shed vortices in a transonic rotor following a wake generator: A comparison betw.Journal of Turbomachinery, ,133 (3 ),

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, ,

Apyan A.; Galbraith D.; Galbraith M.; Orkwis P.; Turner M. (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, ,

Driscoll J.; Eagle E.; Galbraith D.; Galbraith M.; Orkwis P.; Turner M. (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 ),1309-1324

Bruna D.; Dey S.; Gutzwiller D.; Merchant A.; Park K.; Siddappaji K.; Turner M. (12-01-2010. )Framework for multidisciplinary optimization of turbomachinery.Proceedings of the ASME Turbo Expo, ,7 (PARTS A, B, AND C ),623-631

Gutzwiller D.; Turner M. (01-01-2010. )Rapid low fidelity turbomachinery disk optimization.Advances in Engineering Software, ,41 (5 ),779-791

Gorrell S.; List M.; 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 ),

Guidotti E.; Turner M. (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 ),685-698

Downing M.; Gutzwiller D.; Turner M. (12-01-2009. )Educational software for blade and disk design.Proceedings of the ASME Turbo Expo, ,1 ,827-838

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 ),167-179

Gorrell S.; List M.; 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 ),2599-2609

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, ,

Beach T.; Galbraith D.; Knapke R.; List M.; Merchant A.; Turner M. (12-01-2008. )Time accurate simulations of a counter-rotating aspirated compressor.Proceedings of the ASME Turbo Expo, ,6 (PART A ),481-496

Claus R.; Lavelle T.; Reed J.; Townsend S.; Turner M. (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

Bruna D.; Merchant A.; Turner M. (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

Gorrell S.; List M.; Nimersheim J.; Turner M. (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

Galbraith D.; Galbraith M.; List M.; Nimersheim J.; Turner M. (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

Darmofal D.; Keyes D.; Mavriplis 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.; Merchant A.; Turner M. (09-24-2007. )An educational software suite for teaching design strategies for multistage axial flow compressors.Proceedings of the ASME Turbo Expo, ,3 ,465-474

Szabo I.; Turner M. (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

Beach T.; Kamp M.; Nimersheim J.; Turner M. (07-02-2007. )A turbomachinery gridding system .Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting, ,1 ,111-123

Car D.; Gorrell S.; Turner M. (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.; Lavelle T.; Naiman C.; Townsend S.; 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 ,113-122

Bruna D.; Merchant A.; Turner M. (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 ,937-952

Lukovic B.; Orkwis P.; Sekar B.; Turner M. (07-01-2006. )Neural network modeling of deterministic unsteadiness source terms.AIAA Journal, ,44 (7 ),1609-1616

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 ,1127-1136

Car D.; Gorrell S.; Turner M. (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 ,1195-1209

Davis K.; Fowler T.; Islam S.; Kukreti A.; Maltbie C.; Oerther D.; Turner M. (01-01-2005. )Investigating student interest in post-secondary STEM education .ASEE Annual Conference and Exposition, Conference Proceedings, ,9021-9036

Shabbir A.; Turner M. (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

Reed J.; Ryder R.; Turner M.; Veres J. (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

Chen J.; List M.; Remotigue M.; Turner M.; Veres J. (07-01-2004. )Unsteady cooled turbine solutions using a PC-Linux analysis system .AIAA Paper, ,28-39

Norris A.; Turner M.; 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, ,

Caldwell N.; Filz C.; Lee D.; Orkwist P.; Pes M.; Turner M. (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, ,

Adamczyk J.; Celestina M.; Liu N.; Moder J.; Norris A.; Ryder R.; Turner M.; 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, ,

Barter J.; Orkwis P.; Turner M. (01-01-2002. )Linear deterministic source terms for hot streak simulations.Journal of Propulsion and Power, ,18 (2 ),383-389

Barter J.; Orkwis P.; Turner M. (01-01-2000. )Linear deterministic source terms for hot streak simulations.Proceedings of the ASME Turbo Expo, ,1 ,

Kirtley K.; Saeidi S.; Turner M. (01-01-1999. )An average passage closure model for general meshes.Proceedings of the ASME Turbo Expo, ,1 ,

Beach T.; Dailey L.; Hunter S.; Saeidi S.; Topp D.; Turner M.; Vitt P. (01-01-1999. )Multistage simulations of the GE90 turbine.Proceedings of the ASME Turbo Expo, ,1 ,

Turner M. (01-01-1996. )Multistage turbine simulations with vortex-blade interaction.Journal of Turbomachinery, ,118 (4 ),643-653

Chiang H.; Turner M. (01-01-1996. )Compressor blade forced response due to downstream vane-strut potential interaction.Journal of Turbomachinery, ,118 (1 ),134-142

Turner M. (01-01-1995. )Multistage turbine simulations with vortex-blade interaction.Proceedings of the ASME Turbo Expo, ,1 ,

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 ),261-272

Jennions I.; Turner M. (01-01-1993. )An investigation of turbulence modeling in transonic fans including a novel implementation of an imp.Journal of Turbomachinery, ,115 (2 ),249-260

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, ,3B ,

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

Beauchamp P.; Jennions I.; Liang T.; Turner M. (01-01-1993. )The use of orthogonal grids in turbine CFD computations.ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition, GT 1993, ,1 ,

Beachamp P.; Jennions I.; Liang T.; Turner M. (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, ,1 ,

Jennions I.; Turner M. (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, ,1 ,