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Roque Corral (ORCID:0000-0001-9993-6535)
Roque Corral (ORCID:0000-0001-9993-6535)
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Title
Cited by
Cited by
Year
Asymptotic description of maximum mistuning amplification of bladed disk forced response
C Martel, R Corral
Journal of engineering for gas turbines and power 131 (2), 2009
1542009
Stability increase of aerodynamically unstable rotors using intentional mistuning
C Martel, R Corral, JM Llorens
1432008
CO2 emissions from a spark ignition engine operating on natural gas–hydrogen blends (HCNG)
E Navarro, TJ Leo, R Corral
Applied Energy 101, 112-120, 2013
1012013
Efficient edge-based rotor/stator interaction method
MA Burgos, J Contreras, R Corral
AIAA journal 49 (1), 19-31, 2011
842011
Linear and Non-Validation of a Linear Multigrid Accelerated Unstructured Navier-Stokes Solver for the Computation of Turbine Blades on Hybrid Grids
R Corral, A Escribano, F Gisbert, A Serrano, C Vasco
9th AIAA/CEAS Aeroacoustics Conference and Exhibit, 3326, 2003
762003
Profiled end wall design using an adjoint Navier–Stokes solver
R Corral, F Gisbert
712008
The low reduced frequency limit of vibrating airfoils—Part I: Theoretical analysis
R Corral, A Vega
Journal of Turbomachinery 138 (2), 021004, 2016
572016
Aeroelastic stability of welded-in-pair low pressure turbine rotor blades: A comparative study using linear methods
R Corral, JM Gallardo, C Vasco
57*2007
Execution of a parallel edge-based Navier–Stokes solver on commodity graphics processor units
R Corral, F Gisbert, J Pueblas
International Journal of Computational Fluid Dynamics 31 (2), 93-108, 2017
50*2017
Nonlinear dynamics of bladed disks with multiple unstable modes
R Corral, JM Gallardo
AIAA journal 52 (6), 1124-1132, 2014
50*2014
Physics of vibrating turbine airfoils at low reduced frequency
R Corral, A Vega
Journal of Propulsion and Power 32 (2), 325-336, 2016
49*2016
Parallel multigrid unstructured method for the solution of the navier-stokes equations
R Corral, J Crespo, F Gisbert
42nd AIAA Aerospace Sciences Meeting and Exhibit, 761, 2004
462004
Flutter generation and control using mistuning in a turbine rotating rig
R Corral, J Beloki, P Calza, R Elliott
AIAA Journal 57 (2), 782-795, 2019
422019
Flutter amplitude saturation by nonlinear friction forces: Reduced model verification
C Martel, R Corral, R Ivaturi
Journal of Turbomachinery 137 (4), 041004, 2015
402015
Fourier/Chebyshev methods for the incompressible Navier-Stokes equations in infinite domains
R Corral, J Jimenez
Journal of Computational Physics 121 (2), 261-270, 1995
381995
The Low Reduced Frequency Limit of Vibrating Airfoils: Part II — Numerical Experiments
A Vega, R Corral
Journal of Turbomachinery 138 (2), 021005, 2016
372016
Design of mistuning patterns to control the vibration amplitude of unstable rotor blades
R Corral, O Khemiri, C Martel
Aerospace Science and Technology 80, 20-28, 2018
362018
Parametric design of turbomachinery airfoils using highly differentiable splines
R Corral, G Pastor
Journal of Propulsion and Power 20 (2), 335-343, 2004
35*2004
Conceptual Flutter Analysis of Labyrinth Seals Using Analytical Models—Part I: Theoretical Support
R Corral, A Vega
Journal of Turbomachinery 140 (12), 121006, 2018
312018
An implicit harmonic balance method in graphics processing units for oscillating blades
J Crespo, R Corral, J Pueblas
Journal of Turbomachinery 138 (3), 031001, 2016
31*2016
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