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Hanif S. Hoseini
Hanif S. Hoseini
Research Engineer, School of Aerospace Engineering, Georgia Institute of Technology
Correu electrònic verificat a gatech.edu
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Final approach and flare control of a flexible aircraft in crosswind landings
H Sadat-Hoseini, SA Fazelzadeh, A Rasti, P Marzocca
Journal of Guidance, Control, and Dynamics 36 (4), 946-957, 2013
362013
Optimal flutter suppression of nonlinear typical wing section using time-domain finite elements method
SA Fazelzadeh, A Rasti, H Sadat-Hoseini
Journal of Aerospace Engineering 27 (5), 04014028, 2014
132014
Nonlinear flight dynamics of a flexible aircraft subjected to aeroelastic and gust loads
SA Fazelzadeh, H Sadat-Hoseini
Journal of Aerospace Engineering 25 (1), 51-63, 2012
132012
Aeroelastic Stability Analysis of Damaged High-Aspect-Ratio Composite Wings
HS Hoseini, DH Hodges
Journal of Aircraft 56 (5), 1794-1808, 2019
82019
Nonlinear Flutter and Limit-Cycle Oscillations of Damaged Highly Flexible Composite Wings
HS Hoseini, DH Hodges
Nonlinear Dynamics 97 (1), 247-268, 2019
82019
A Joined 3D/1D Finite Element Method for Aeroservoelastic Analysis of Damaged HALE Aircraft Wings
HS Hoseini
Georgia Institute of Technology, 2018
52018
Flutter suppression for finite element modeling of damaged hale aircraft wings
H Hoseini, DH Hodges
2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2018
52018
Nonlinear Aeroelastic Analysis of High Aspect Ratio Wings Using Joined 3D Finite Elements and Variational Asymptotic Beam Models
H Hoseini, DH Hodges
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2017
52017
Joining 3D Finite Elements to Variational Asymptotic Beam Models
HS Hoseini, DH Hodges
57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2016
52016
Flutter Suppression For Damaged High-Aspect-Ratio Wings: Implementation in Abaqus
HS Hoseini, DH Hodges
AIAA Journal 57 (10), 4354-4367, 2019
22019
En aquests moments el sistema no pot dur a terme l'operació. Torneu-ho a provar més tard.
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