Jack McNamara

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Citations	3706	1981
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Rohit DeshmukhFlorida Atlantic UniversityVerified email at buckeyemail.osu.edu
Vilas ShindeDepartment of Aerospace Engineering at Mississippi State UniversityVerified email at ae.msstate.edu
Zachary RileyAir Force Research LaboratoryVerified email at us.af.mil
Miguel VisbalAir Force Research LaboratoryVerified email at us.af.mil
XQ WangArizona State UniversityVerified email at asu.edu
Bryan GlazU.S. Army Research LaboratoryVerified email at army.mil
Benjamin GrierClemson University, The Ohio State UniversityVerified email at osu.edu
Michael Oppenheimerair force research laboratoryVerified email at woh.rr.com
David B. Doman_________________________________________________Verified email at woh.rr.com
Carlos E. S. CesnikClarence L. "Kelly" Johnson Professor of Aerospace Engineering, The University of MichiganVerified email at umich.edu
Stephen Michael NogarPost Doctoral Researcher, U.S. Army Research LaboratoryVerified email at mail.mil
Andrea SerraniThe Ohio State UniversityVerified email at osu.edu
Zongxian LiangFlow Science Inc.Verified email at flow3d.com
Troy ShiltSandia National LaboratoriesVerified email at sandia.gov
Nicolas LamorteUniversity of MichiganVerified email at umich.edu
Kelsey ShalerNational Renewable Energy LaboratoryVerified email at nrel.gov
Zico KolterCarnegie Mellon UniversityVerified email at cs.cmu.edu
Raghavendra MurthyAssistant Teaching Professor, Arizona State UniversityVerified email at asu.edu
Joseph ConnollyNASAVerified email at nasa.gov
George KopasakisSenior Research Engineer, NASA GRCVerified email at nasa.gov

Jack McNamara

Professor, Mechanical & Aerospace Engineering, The Ohio State University

Verified email at osu.edu

Multiphysics Interactions of Aerospace Systems (e.g. fluid/structure fluid/thermal/structural fluid/structural/control etc).


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Aeroelastic and aerothermoelastic analysis in hypersonic flow: past, present, and future JJ McNamara, PP Friedmann AIAA journal 49 (6), 1089-1122, 2011	379	2011
Studies on fluid-thermal-structural coupling for aerothermoelasticity in hypersonic flow AJ Culler, JJ McNamara AIAA journal 48 (8), 1721-1738, 2010	276	2010
Impact of fluid-thermal-structural coupling on response prediction of hypersonic skin panels AJ Culler, JJ McNamara AIAA journal 49 (11), 2393-2406, 2011	157	2011
Reduced-order aerothermoelastic framework for hypersonic vehicle control simulation NJ Falkiewicz, CES Cesnik, AR Crowell, JJ McNamara AIAA journal 49 (8), 1625-1646, 2011	143	2011
Aeroelastic and aerothermoelastic analysis of hypersonic vehicles: current status and future trends J McNamara, P Friedmann 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2007	143	2007
Approximate modeling of unsteady aerodynamics for hypersonic aeroelasticity JJ McNamara, AR Crowell, PP Friedmann, B Glaz, A Gogulapati Journal of Aircraft 47 (6), 1932-1945, 2010	136	2010
Aeroelastic and aerothermoelastic behavior in hypersonic flow JJ McNamara, PP Friedmann, KG Powell, BJ Thuruthimattam, RE Bartels AIAA journal 46 (10), 2591-2610, 2008	110	2008
Flutter boundary identification for time-domain computational aeroelasticity JJ McNamara, PP Friedmann AIAA journal 45 (7), 1546-1555, 2007	96	2007
Model reduction of computational aerothermodynamics for hypersonic aerothermoelasticity AR Crowell, JJ McNamara AIAA journal 50 (1), 74-84, 2012	92	2012
The impact of flow induced loads on snap-through behavior of acoustically excited, thermally buckled panels BA Miller, JJ McNamara, SM Spottswood, AJ Culler Journal of sound and vibration 330 (23), 5736-5752, 2011	85	2011
Aeroelastic analysis of hypersonic vehicles PP Friedmann, JJ McNamara, BJ Thuruthimattam, I Nydick Journal of Fluids and Structures 19 (5), 681-712, 2004	68	2004
Hypersonic aerothermoelastic response prediction of skin panels using computational fluid dynamic surrogates AR Crowell, J McNamara, B Miller Journal of Aeroelasticity and Structural Dynamics 2 (2), 2011	65	2011
Uncertainty propagation in hypersonic aerothermoelastic analysis N Lamorte, PP Friedmann, B Glaz, AJ Culler, AR Crowell, JJ McNamara Journal of Aircraft 51 (1), 192-203, 2014	64	2014
Response of a panel to shock impingement: Modeling and comparison with experiments-part 2 A Gogulapati, R Deshmukh, JJ McNamara, V Vyas, XQ Wang, ... 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2015	60	2015
Aeroelastic and aerothermoelastic behavior of two and three dimensional lifting surfaces in hypersonic flow JJ McNamara University of Michigan, 2005	60	2005
Interplay of surface deformation and shock-induced separation in shock/boundary-layer interactions KR Brouwer, A Gogulapati, JJ McNamara AIAA Journal 55 (12), 4258-4273, 2017	58	2017
Three-dimensional aeroelastic and aerothermoelastic behavior in hypersonic flow J McNamara, P Friedmann, K Powell, B Thuruthimattam, R Bartels 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials …, 2005	55	2005
Response of a panel to shock impingement: modeling and comparison with experiments A Gogulapati, R Deshmukh, AR Crowell, JJ McNamara, V Vyas, XQ Wang, ... 55th AIAA/ASMe/ASCE/AHS/SC Structures, Structural Dynamics, and Materials …, 2014	54	2014
Performance enhancement and load reduction of a 5 MW wind turbine blade RW Vesel Jr, JJ McNamara Renewable energy 66, 391-401, 2014	53	2014
Enriched piston theory for expedient aeroelastic loads prediction in the presence of shock impingements KR Brouwer, JJ McNamara AIAA Journal 57 (3), 1288-1302, 2019	49	2019

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