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Jack J. McNamara, Ph.D. - Publications

Affiliations: 
2005 University of Michigan, Ann Arbor, Ann Arbor, MI 
Area:
Aerospace Engineering
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43 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 Brouwer KR, McNamara JJ. Generalized Treatment of Surface Deformation for High-Speed Computational Fluid Dynamic Surrogates Aiaa Journal. 58: 329-340. DOI: 10.2514/1.J058470  0.329
2020 Connolly JW, Kopasakis G, Chwalowski P, Carlson J, Sanetrik MD, Silva WA, McNamara J. Aero-Propulso-Elastic Analysis of a Supersonic Transport Journal of Aircraft. 57: 569-585. DOI: 10.2514/1.C035531  0.31
2020 Brouwer KR, McNamara JJ. Surrogate-based aeroelastic loads prediction in the presence of shock-induced separation Journal of Fluids and Structures. 93: 102838. DOI: 10.1016/J.Jfluidstructs.2019.102838  0.42
2020 Shilt T, O’Hara PJ, Deshmukh R, McNamara JJ. Solution of nearly incompressible field problems using a generalized finite element approach Computer Methods in Applied Mechanics and Engineering. 368: 113165. DOI: 10.1016/J.Cma.2020.113165  0.302
2020 Shinde V, McNamara J, Gaitonde D. Control of transitional shock wave boundary layer interaction using structurally constrained surface morphing Aerospace Science and Technology. 96: 105545. DOI: 10.1016/J.Ast.2019.105545  0.581
2020 Deshmukh R, Shilt T, McNamara JJ. Efficient representation of turbulent flows using data-enriched finite elements International Journal For Numerical Methods in Engineering. 121: 3397-3416. DOI: 10.1002/Nme.6364  0.33
2019 Brouwer KR, McNamara JJ. Enriched Piston Theory for Expedient Aeroelastic Loads Prediction in the Presence of Shock Impingements Aiaa Journal. 57: 1288-1302. DOI: 10.2514/1.J057595  0.306
2019 Shaler K, Kecskemety KM, McNamara JJ. Benchmarking of a Free Vortex Wake Model for Prediction of Wake Interactions Renewable Energy. 136: 607-620. DOI: 10.1016/J.Renene.2018.12.044  0.308
2019 Shinde V, McNamara J, Gaitonde D, Barnes C, Visbal M. Transitional shock wave boundary layer interaction over a flexible panel Journal of Fluids and Structures. 90: 263-285. DOI: 10.1016/J.Jfluidstructs.2019.07.007  0.581
2018 Miller BA, McNamara JJ. Efficient Fluid-Thermal-Structural Time Marching with Computational Fluid Dynamics Aiaa Journal. 56: 3610-3621. DOI: 10.2514/1.J056572  0.324
2018 Nogar SM, Serrani A, Gogulapati A, McNamara JJ, Oppenheimer MW, Doman DB. Design and Evaluation of a Model-Based Controller for Flapping-Wing Micro Air Vehicles Journal of Guidance Control and Dynamics. 41: 2513-2528. DOI: 10.2514/1.G003293  0.311
2018 Boyer NR, McNamara J, Gaitonde D, Barnes CJ, Visbal MR. Features of shock-induced panel flutter in three-dimensional inviscid flow Journal of Fluids and Structures. 83: 490-506. DOI: 10.1016/J.Jfluidstructs.2018.10.001  0.578
2018 Deshmukh R, McNamara JJ, Kolter JZ. Energy balance of reduced order models for unsteady flows using sparse coding Nonlinear Dynamics. 94: 197-210. DOI: 10.1007/S11071-018-4353-4  0.33
2017 Brouwer KR, Gogulapati A, McNamara JJ. Interplay of Surface Deformation and Shock-Induced Separation in Shock/Boundary-Layer Interactions Aiaa Journal. 55: 4258-4273. DOI: 10.2514/1.J056030  0.36
2017 Riley ZB, McNamara JJ. Interaction Between Compliant Structures and Boundary-Layer Transition in Hypersonic Flow Aiaa Journal. 55: 2645-2663. DOI: 10.2514/1.J055521  0.368
2017 Nogar SM, Gogulapati A, McNamara JJ, Serrani A, Oppenheimer MW, Doman DB. Control-Oriented Modeling of Coupled Electromechanical-Aeroelastic Dynamics for Flapping-Wing Vehicles Journal of Guidance Control and Dynamics. 40: 1664-1679. DOI: 10.2514/1.G002503  0.349
2016 LaFontaine JH, Gogulapati A, McNamara JJ, Silva WA. Effects of strain hardening on response of skin panels in hypersonic flow Aiaa Journal. 54: 1974-1986. DOI: 10.2514/1.J054582  0.336
2016 Deshmukh R, McNamara JJ, Liang Z, Kolter JZ, Gogulapati A. Model order reduction using sparse coding exemplified for the lid-driven cavity Journal of Fluid Mechanics. 808: 189-223. DOI: 10.1017/Jfm.2016.616  0.343
2016 Kecskemety KM, McNamara JJ. Influence of wake dynamics on the performance and aeroelasticity of wind turbines Renewable Energy. 88: 333-345. DOI: 10.1016/J.Renene.2015.11.031  0.352
2016 Riley ZB, McNamara JJ. Interaction between aerothermally compliant structures and boundary layer transition in hypersonic flow 15th Dynamics Specialists Conference.  0.306
2016 Boyer NR, McNamara JJ, Visbal MR. Study on shock-induced panel flutter in 2-D laminar flow 15th Dynamics Specialists Conference.  0.324
2016 Brouwer KR, Gogulapati A, McNamara JJ. Efficient treatment of structural deformation for aerothermoelastic loads prediction in high-speed flows 15th Dynamics Specialists Conference.  0.305
2015 Riley ZB, Deshmukh R, Miller BA, McNamara JJ. Characterization of structural response to hypersonic boundary layer transition 56th Aiaa/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference. DOI: 10.2514/1.J054607  0.436
2015 Brouwer KR, Crowell AR, McNamara JJ. Rapid prediction of unsteady aeroelastic loads in shock-dominated flows 56th Aiaa/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference.  0.354
2014 Riley ZB, McNamara JJ, Johnson HB. Assessing hypersonic boundary-layer stability in the presence of structural deformation Aiaa Journal. 52: 2547-2558. DOI: 10.2514/1.J052941  0.354
2014 Lamorte N, Friedmann PP, Glaz B, Culler AJ, Crowell AR, McNamara JJ. Uncertainty propagation in hypersonic aerothermoelastic analysis Journal of Aircraft. 51: 192-203. DOI: 10.2514/1.C032233  0.373
2014 Vesel RW, McNamara JJ. Performance enhancement and load reduction of a 5MW wind turbine blade Renewable Energy. 66: 391-401. DOI: 10.1016/J.Renene.2013.12.019  0.318
2013 Crowell AR, Miller BA, McNamara JJ. Robust and efficient treatment of temperature feedback in fluid-thermal-structural analysis Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. DOI: 10.2514/1.J052820  0.394
2013 Deshmukh R, McNamara JJ, Culler AJ. Response of skin panels to combined self and boundary layer induced fluctuating pressure 54th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference. DOI: 10.1016/J.Jfluidstructs.2015.08.008  0.381
2012 Crowell AR, McNamara JJ. Model reduction of computational aerothermodynamics for hypersonic aerothermoelasticity Aiaa Journal. 50: 74-84. DOI: 10.2514/1.J051094  0.395
2012 Miller BA, Crowell AR, Mcnamara JJ. Modeling and analysis of shock impingements on thermo-mechanically compliant surface panels Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference.  0.332
2012 Miller BA, Crowell AR, Mcnamara JJ. Modeling and analysis of shock impingements on thermo-mechanically compliant surface panels Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference.  0.332
2011 Crowell AR, Miller BA, McNamara JJ. Computational modeling for conjugate heat transfer of shock-surface interactions on compliant skin panels Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. DOI: 10.2514/6.2011-2017  0.329
2011 Culler AJ, McNamara JJ. Impact of fluid-thermal-structural coupling on response prediction of hypersonic skin panels Aiaa Journal. 49: 2393-2406. DOI: 10.2514/1.J050617  0.393
2011 Ng WH, Friedmann PP, Waas AM, McNamara JJ. Thermomechanical behaviour of a damaged thermal protection system: experimental correlation and influence of hypersonic flow The Aeronautical Journal. 115: 69-82. DOI: 10.1017/S0001924000005467  0.368
2010 Kecskemety KM, McNamara JJ. The influence of wake effects and inflow turbulence on wind turbine loads Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. DOI: 10.2514/1.J051095  0.353
2010 Culler AJ, McNamara JJ. Studies on fluid-thermal-structural coupling for aerothermoelasticity in hypersonic flow Aiaa Journal. 48: 1721-1738. DOI: 10.2514/1.J050193  0.392
2010 McNamara JJ, Crowell AR, Friedmann PP, Glaz B, Gogulapati A. Approximate modeling of unsteady aerodynamics for hypersonic aeroelasticity Journal of Aircraft. 47: 1932-1945. DOI: 10.2514/1.C000190  0.364
2010 Miller BA, McNamara JJ, Culler AJ, Spottswood SM. The impact of flow induced loads on snap-through behavior of acoustically excited, thermally buckled panels Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. DOI: 10.1016/J.Jsv.2011.06.028  0.42
2009 McNamara JJ, Culler AJ, Crowell AR. Aerothermoelastic modeling considerations for hypersonic vehicles 16th Aiaa/Dlr/Dglr International Space Planes and Hypersonic Systems and Technologies Conference.  0.307
2008 McNamara JJ, Friedmann PP, Powell KG, Thuruthimattam BJ, Bartels RE. Aeroelastic and aerothermoelastic behavior in hypersonic flow Aiaa Journal. 46: 2591-2610. DOI: 10.2514/1.36711  0.63
2007 McNamara JJ, Friedmann PP. Flutter-boundary identification for time-domain computational aeroelasticity Aiaa Journal. 45: 1546-1555. DOI: 10.2514/1.26706  0.373
2004 Friedmann PP, McNamara JJ, Thuruthimattam BJ, Nydick I. Aeroelastic analysis of hypersonic vehicles Journal of Fluids and Structures. 19: 681-712. DOI: 10.1016/J.Jfluidstructs.2004.04.003  0.368
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