Bret Stanford

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Philip BeranPrincipal Research Aerospace Engineer, Air Force Research LaboratoryE-mail confirmado em us.af.mil
Pin WuE-mail confirmado em ufl.edu
Carlos E. S. CesnikClarence L. "Kelly" Johnson Professor of Aerospace Engineering, The University of MichiganE-mail confirmado em umich.edu
James HubnerProfessor, University of AlabamaE-mail confirmado em eng.ua.edu
Hyunsun Alicia KimUC San DiegoE-mail confirmado em ucsd.edu
Peter DunningLecturer, University of AberdeenE-mail confirmado em abdn.ac.uk
Mohammad H. KurdiFord Motor CompanyE-mail confirmado em ford.com
Lawrence UkeileyUniversity of FloridaE-mail confirmado em ufl.edu
Satish Kumar Chimakurthi, Ph.D.President and CEO of Epitome Research and Innovations Inc.E-mail confirmado em epitomeri.com
Vijay JagdaleSenior Engineer / Research Scientist, United Technologies Research Center, East Hartford, CTE-mail confirmado em utrc.utc.com
Manav BhatiaMississippi State UniversityE-mail confirmado em msstate.edu
Mayuresh PatilGeorgia TechE-mail confirmado em gatech.edu
Yongsheng LianUniversity of LouisvilleE-mail confirmado em louisville.edu
Pat TrizilaE-mail confirmado em umich.edu
Liu HaoMoffitt Cancer CenterE-mail confirmado em moffitt.org
Mujahid AbdulrahimUniversity of Missouri Kansas CityE-mail confirmado em umkc.edu
Craig WoolseyAerospace & Ocean Engineering, Virginia TechE-mail confirmado em vt.edu
Hikaru AonoDepartment of Mechanical Engineering and Robotics, Shinshu UniversityE-mail confirmado em shinshu-u.ac.jp
BV SankarUniversity of FloridaE-mail confirmado em ufl.edu
Paul M WeaverBernal Chair in Composite Structures, Uni Limerick; Prof. in Lightweight Structures, Uni Bristol;E-mail confirmado em ul.ie

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Bret Stanford

NASA Langley Research Center

E-mail confirmado em nasa.gov


Título Ordenar por citações Ordenar por ano Ordenar por título	Citado por Citado por	Ano
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	212	2008
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	210	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	170	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	149	2010
Optimal topology of aircraft rib and spar structures under aeroelastic loads BK Stanford, PD Dunning Journal of Aircraft 52 (4), 1298-1311, 2015	120	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	108	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	90	2012
Aeroelastic topology optimization of membrane structures for micro air vehicles B Stanford, P Ifju Structural and Multidisciplinary Optimization 38, 301-316, 2009	89	2009
Uncertainty quantification in aeroelasticity P Beran, B Stanford, C Schrock Annual review of fluid mechanics 49 (1), 361-386, 2017	83	2017
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	83	2007
Aeroelastic benefits of tow steering for composite plates BK Stanford, CV Jutte, KC Wu Composite Structures 118, 416-422, 2014	81	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
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	68	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	65	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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