Bret Stanford

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Philip BeranPrincipal Research Aerospace Engineer, Air Force Research LaboratoryVerified email at us.af.mil
Pin WuVerified email at ufl.edu
Carlos E. S. CesnikClarence L. "Kelly" Johnson Professor of Aerospace Engineering, The University of MichiganVerified email at umich.edu
James HubnerProfessor, University of AlabamaVerified email at eng.ua.edu
Hyunsun Alicia KimUC San DiegoVerified email at ucsd.edu
Peter DunningLecturer, University of AberdeenVerified email at abdn.ac.uk
Mohammad H. KurdiFord Motor CompanyVerified email at ford.com
Lawrence UkeileyUniversity of FloridaVerified email at ufl.edu
Satish Kumar Chimakurthi, Ph.D.President and CEO of Epitome Research and Innovations Inc.Verified email at epitomeri.com
Vijay JagdaleSenior Engineer / Research Scientist, United Technologies Research Center, East Hartford, CTVerified email at utrc.utc.com
Manav BhatiaMississippi State UniversityVerified email at msstate.edu
Mayuresh PatilGeorgia TechVerified email at gatech.edu
Yongsheng LianUniversity of LouisvilleVerified email at louisville.edu
Pat TrizilaVerified email at umich.edu
Liu HaoMoffitt Cancer CenterVerified email at moffitt.org
Mujahid AbdulrahimUniversity of Missouri Kansas CityVerified email at umkc.edu
Craig WoolseyAerospace & Ocean Engineering, Virginia TechVerified email at vt.edu
Hikaru AonoDepartment of Mechanical Engineering and Robotics, Shinshu UniversityVerified email at shinshu-u.ac.jp
BV SankarUniversity of FloridaVerified email at ufl.edu
Paul M WeaverBernal Chair in Composite Structures, Uni Limerick; Prof. in Lightweight Structures, Uni Bristol;Verified email at ul.ie

Bret Stanford

NASA Langley Research Center

Verified email at nasa.gov


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Computational aerodynamics of low Reynolds number plunging, pitching and flexible wings for MAV applications W Shyy, Y Lian, J Tang, H Liu, P Trizila, B Stanford, L Bernal, C Cesnik, ... Acta Mechanica Sinica 24, 351-373, 2008	209	2008
Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring B Stanford, P Ifju, R Albertani, W Shyy Progress in Aerospace Sciences 44 (4), 258-294, 2008	207	2008
Aerodynamic coefficients and deformation measurements on flexible micro air vehicle wings R Albertani, B Stanford, JP Hubner, PG Ifju Experimental Mechanics 47, 625-635, 2007	167	2007
Analytical sensitivity analysis of an unsteady vortex-lattice method for flapping-wing optimization BK Stanford, PS Beran Journal of Aircraft 47 (2), 647-662, 2010	147	2010
Optimal topology of aircraft rib and spar structures under aeroelastic loads BK Stanford, PD Dunning Journal of Aircraft 52 (4), 1298-1311, 2015	114	2015
Flapping wing structural deformation and thrust correlation study with flexible membrane wings P Wu, P Ifju, B Stanford AIAA journal 48 (9), 2111-2122, 2010	106	2010
Global optimization of actively morphing flapping wings M Ghommem, MR Hajj, DT Mook, BK Stanford, PS Beran, RD Snyder, ... Journal of Fluids and Structures 33, 210-228, 2012	89	2012
Aeroelastic topology optimization of membrane structures for micro air vehicles B Stanford, P Ifju Structural and Multidisciplinary Optimization 38, 301-316, 2009	88	2009
Static aeroelastic model validation of membrane micro air vehicle wings B Stanford, M Sytsma, R Albertani, D Viieru, W Shyy, P Ifju AIAA journal 45 (12), 2828-2837, 2007	82	2007
Aeroelastic benefits of tow steering for composite plates BK Stanford, CV Jutte, KC Wu Composite Structures 118, 416-422, 2014	80	2014
Investigation of membrane actuation for roll control of a micro air vehicle B Stanford, M Abdulrahim, R Lind, P Ifju Journal of Aircraft 44 (3), 741-749, 2007	80	2007
Uncertainty quantification in aeroelasticity P Beran, B Stanford, C Schrock Annual review of fluid mechanics 49 (1), 361-386, 2017	79	2017
Structural dynamics and aerodynamics measurements of biologically inspired flexible flapping wings P Wu, BK Stanford, E Sällström, L Ukeiley, PG Ifju Bioinspiration & biomimetics 6 (1), 016009, 2011	77	2011
Comparison of curvilinear stiffeners and tow steered composites for aeroelastic tailoring of aircraft wings BK Stanford, CV Jutte Computers & Structures 183, 48-60, 2017	67	2017
Coupled aerostructural topology optimization using a level set method for 3D aircraft wings PD Dunning, BK Stanford, HA Kim Structural and Multidisciplinary Optimization 51, 1113-1132, 2015	67	2015
Aeroelastic topology optimization of blade-stiffened panels B Stanford, P Beran, M Bhatia Journal of Aircraft 51 (3), 938-944, 2014	64	2014
Aeroelastic tailoring of transport aircraft wings: state-of-the-art and potential enabling technologies C Jutte, BK Stanford	63	2014
Direct flutter and limit cycle computations of highly flexible wings for efficient analysis and optimization B Stanford, P Beran Journal of Fluids and Structures 36, 111-123, 2013	62	2013
A computational and experimental studies of flexible wing aerodynamics H Aono, SK Chimakurthi, P Wu, E Sallstrom, B Stanford, C Cesnik, P Ifju, ... 48th AIAA aerospace sciences meeting including the new horizons forum and …, 2010	61	2010
Aeroelastic tailoring of the NASA common research model via novel material and structural configurations CV Jutte, B Stanford, CD Wieseman, JB Moore 52nd aerospace sciences meeting, 0598, 2014	55	2014

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