Haddad Khodaparast, H
16  results:
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1

The effect of folding wingtips on the worst-case gust loads..:

Balatti, D ; Haddad Khodaparast, H ; Friswell, M. I..
https://openaccess.city.ac.uk/id/eprint/27038/1/09544100211010915.pdf.  , 2022
 
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2

Aircraft turbulence and gust identification using simulated..:

Balatti, D ; Haddad Khodaparast, H ; Friswell, M. I..
https://openaccess.city.ac.uk/id/eprint/26988/1/1-s2.0-S1270963821003151-main.pdf.  , 2021
 
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3

An equivalent model of a nonlinear bolted flange joint:

Jamia, N ; Jalali, Hassan ; Taghipour, J..
https://nrl.northumbria.ac.uk/id/eprint/45031/1/1-s2.0-S0888327020308931-main.pdf.  , 2021
 
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4

Aeroelastic stability analysis of aircraft wings with initi..:

Amoozgar, M. R ; Fazelzadeh, S. A ; Haddad Khodaparast, H..
Amoozgar , M R , Fazelzadeh , S A , Haddad Khodaparast , H , Friswell , M I & Cooper , J E 2020 , ' Aeroelastic stability analysis of aircraft wings with initial curvature ' , Aerospace Science and Technology , vol. 107 , 106241 . https://doi.org/10.1016/j.ast.2020.106241.  , 2020
 
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5

Conceptual-level evaluation of a variable stiffness skin fo..:

Wang, C ; Haddad Khodaparast, H ; Friswell, MI...
info:eu-repo/semantics/altIdentifier/wos/WOS:000490896900017.  , 2019
 
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7

Fuzzy finite element model updating of the DLR AIRMOD test ..:

Haddad Khodaparast, H ; Govers, Y ; Dayyani, Iman...
Haddad Khodaparast H, Govers Y, Dayyani I, Adhikari S, Link M, Friswell MI, Mottershead JE, Sienz J, Fuzzy finite element model updating of the DLR AIRMOD test structure, Vol. 52, December 2017, pp. 512-526.  , 2017
 
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12

Stochastic modelling and updating of a joint contact interf..:

Jalali, Hassan ; Khodaparast, H. Haddad ; Madinei, H.
https://nrl.northumbria.ac.uk/id/eprint/43883/1/jalali2019%282%29%20%281%29.pdf.  , 2019
 
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