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Shahrokh Shahpar
Shahrokh Shahpar
Rolls-Royce Fellow, Aerothermal Design System
Verified email at rolls-royce.com
Title
Cited by
Cited by
Year
Nonaxisymmetric turbine end wall design: part I—three-dimensional linear design system
NW Harvey, MG Rose, MD Taylor, S Shahpar, J Hartland, ...
J. Turbomach. 122 (2), 278-285, 2000
3142000
PADRAM: Parametric design and rapid meshing system for turbomachinery optimisation
S Shahpar, L Lapworth
Turbo Expo: Power for Land, Sea, and Air 36894, 579-590, 2003
2272003
Robust design using bayesian monte carlo
A Kumar, PB Nair, AJ Keane, S Shahpar
International Journal for Numerical Methods in Engineering 73 (11), 1497-1517, 2008
782008
PADRAM: Parametric design and rapid meshing system for complex turbomachinery configurations
A Milli, S Shahpar
Turbo Expo: Power for Land, Sea, and Air 44748, 2135-2148, 2012
692012
Guide vane for a gas turbine engine
S Shahpar, MD Taylor
US Patent 6,755,612, 2004
682004
Soft: A new design and optimisation tool for turbomachinery
S Shahpar
Evolutionary Methods for Design, Optimisation and Control, 2002
652002
Multi-fidelity design optimisation of a transonic compressor rotor
CJ Brooks, AIJ Forrester, AJ Keane, S Shahpar
622011
A comparative study of optimisation methods for aerodynamic design of turbomachinery blades
S Shahpar
Turbo expo: power for land, sea, and air 78545, V001T03A087, 2000
622000
Turbomachinery design optimization using automatic differentiated adjoint code
MC Duta, S Shahpar, MB Giles
Turbo Expo: Power for Land, Sea, and Air 47950, 1435-1444, 2007
612007
Robust design of compressor fan blades against erosion
A Kumar, AJ Keane, PB Nair, S Shahpar
602006
Leakage uncertainties in compressors: The case of rotor 37
P Seshadri, GT Parks, S Shahpar
Journal of Propulsion and Power 31 (1), 456-466, 2015
562015
Aerodynamic optimization of high-pressure turbines for lean-burn combustion system
S Shahpar, S Caloni
Journal of Engineering for Gas turbines and Power 135 (5), 055001, 2013
542013
Robust compressor blades for desensitizing operational tip clearance variations
P Seshadri, S Shahpar, GT Parks
Turbo Expo: Power for Land, Sea, and Air 45608, V02AT37A043, 2014
512014
SOPHY: An integrated CFD based automatic design optimisation system
S Shahpar
ROLLS ROYCE PLC-REPORT-PNR 93022, 2005
452005
Turbomachinery active subspace performance maps
P Seshadri, S Shahpar, P Constantine, G Parks, M Adams
Journal of Turbomachinery 140 (4), 041003, 2018
442018
Stator vane assembly for a turbomachine
S Shahpar
US Patent 7,118,331, 2006
442006
Novel compressor blade shaping through a free-form method
A John, S Shahpar, N Qin
Journal of Turbomachinery 139 (8), 081002, 2017
392017
Multi-objective design and optimisation of bypass outlet-guide vanes
S Shahpar, D Giacche, L Lapworth
Turbo Expo: Power for Land, Sea, and Air 36894, 591-601, 2003
372003
Design of gas turbine engines using CFD
L Lapworth, S Shahpar
Proceedings of the ECCOMAS 2004, 2004
342004
A computational fluid dynamic acoustic investigation of a tiltwing eVTOL concept aircraft
RJ Higgins, GN Barakos, S Shahpar, I Tristanto
Aerospace Science and Technology 111, 106571, 2021
332021
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