Observatorio de I+D+i UPM
• ESPAÑOL
• ENGLISH
INVESTIGADORES
ESTRUCTURAS DE I+D+I
ACTIVIDAD INVESTIGADORA
INNOVACIÓN
Investigador
Roque Corral Garcia
Categoría Investigador
TITULAR UNIVERSIDAD
Sexo:
V
Escuela UPM
E.T.S.I. AERONÁUTICA Y DEL ESPACIO
Departamento:
MECÁNICA DE FLUIDOS Y PROPULSIÓN AEROESPACIAL (N)
Area Conocimiento
INGENIERIA AEROESPACIAL
Grupo de Investigación:
Sin grupo de investigación
Email (Directorio UPM)
roque.corral
upm.es
Teléfono (Directorio UPM)
639410989
Datos de Memorias relacionados
Proyectos de I+D+i y generación de recursos
19 Proyectos de I+D+i
1: (2009)
ANALISIS DE PROBLEMAS AEROELASTICOS EN TURBOMAQUINARIA MEDIANTE SIMULACIONES NO-LINEALES EFICIENTES
2: (2009)
DESARROLLO DE MÉTODOS NUMÉRICOS Y METODOLOGÍAS PARA EL ANÁLISIS AERODINÁMICO DE TURBOMÁQUINAS.
3: (2009)
N. 030874 - AST5 - CT-2006-030874. - MAGPI.
4: (2009)
OPENAIR Optimisation for low environmental noise impact aircraft
5: (2009)
211861 - VALIDATION OF RADICAL ENGINE ARCHITECTURA SYSTEM (DREAM).
6: (2010)
ANALISIS DE PROBLEMAS AEROELASTICOS EN TURBOMAQUINARIA MEDIANTE SIMULACIONES NO-LINEALES EFICIENTES
7: (2010)
AST5-CT-2006-030939 - TATMO
8: (2010)
DESARROLLO DE MÉTODOS NUMÉRICOS Y METODOLOGÍAS PARA EL ANÁLISIS AERODINÁMICO DE TURBOMÁQUINAS.
9: (2010)
N. 030874 - AST5 - CT-2006-030874. - MAGPI.
10: (2010)
Nº 233799 - ERICKA
11: (2010)
OPENAIR Optimisation for low environmental noise impact aircraft
12: (2010)
211861 - VALIDATION OF RADICAL ENGINE ARCHITECTURA SYSTEM (DREAM).
13: (2011)
DREAM: Validation of radical engine architecture systems
14: (2011)
ERICKA: Engine Representative Internal Cooling Knowledge and Applications
15: (2011)
MAGPI: MAGPI: Main Annulus Gas Path Interactions
16: (2011)
OPENAIR: OPtimisation for low Environmental Noise impact AIRcraft
17: (2014)
DESARROLLO DE MÉTODOS NUMÉRICOS PARA LA SIMULACIÓN DE FENÓMENOS AEROMECÁNICOS EN COMPRESORES
18: (2014)
NUEVAS TÉCNICAS PARA EL ANÁLISIS DE PROBLEMAS DE VIBRACIONES AEROMECÁNICAS EN TURBINAS DE GAS AERONAÚTICAS
19: (2015)
VIBTURB: Nuevas Técnicas para el Análisis de Problemas de Vibraciones Aeromecánicas en Turbinas de Gas Aeronáuticas
Formación de Investigadores y Movilidad
2 Tesis Doctorales
1: (2007)
"Resolution of the Adjoint Navier-Stokes Equations Using a Preconditioned Multigrid Method" o "Resolución de las ecuaciones de Navier-Stokes adjuntas mediante un método multimalla precondicionado"
2: (2015)
ASYMPTOTIC AND COMPUTATIONAL ANALYSIS OF MISTUNING EFFECTS ON THE DYNAMICS OF BLADED DISKS
Difusión de Resultados de Investigación
20 Artículos en revistas
1: (2007)
Aeroelastic stability of welded-in-pair low pressure turbine rotor blades: A comparative study using linear methods
2: (2010)
Optimisation of axially segmented liners for aeroengine broadband noise
3: (2012)
ASYMPTOTIC DESCRIPTION OF FLUTTER AMPLITUDE SATURATION BY NONLINEAR FRICTION FORCES
4: (2012)
FORCED RESPONSE OF BLADED DISKS WITH DAMPING MISTUNING
5: (2013)
Asymptotic description of damping mistuning effects on the forced response of turbomachinery bladed disks
6: (2014)
A case study on optimum tip speed ratio and pitch angle laws for wind turbine rotors operating in yawed conditions
7: (2014)
A STUDY ON THE EFFECTS OF GEOMETRIC NON LINEARITIES ON THE UN-RUNNING TRANSFORMATION OF COMPRESSOR BLADES
8: (2014)
EXPERIMENTAL AND NUMERICAL ASSESSMENT OF THE AEROELASTIC STABILITY OF BLADE PAIR PACKAGES
9: (2014)
FLUTTER AMPLITUDE SATURATION BY NONLINEAR FRICTION FORCES: REDUCED MODEL VALIDATION
10: (2014)
Flutter Amplitude Saturation by Nonlinear Friction Forces: Reduced Model Verification
11: (2014)
Forced Response of Mistuned Bladed Disks: Quantitative Validation of the Asymptotic Description
12: (2014)
Forced Response of Mistuned Bladed Disks: Quantitative Validation of the Asymptotic Description
13: (2014)
Multiphononon resonant Raman scattering in He+-implanted InGaN
14: (2014)
On the effects of windbreaks on the aerodynamic loads over parabolic solar troughs
15: (2014)
Scaling of velocity fluctuations in off-wall boundary conditions for turbulent flows
16: (2015)
A NOVEL MIXING PLANE METHOD USING NON-REFLECTING BOUNDARY CONDITIONS FOR MULTI-ROW ANALYSIS IN TURBOMACHINES
17: (2015)
AN IMPLICIT HARMONIC BALANCE METHOD IN GRAPHICS PROCESSING UNITS FOR VIBRATING BLADES
18: (2015)
Flutter Amplitude Saturation by Nonlinear Friction Forces: Reduced Model Verification
19: (2015)
THE LOW REDUCED FREQUENCY LIMIT OF VIBRATING AIRFOILS. PART I: THEORETICAL ANALYSIS
20: (2015)
THE LOW REDUCED FREQUENCY LIMIT OF VIBRATING AIRFOILS. PART II: NUMERICAL EXPERIMENTS
4 Capítulos de libros
1: (2015)
The Low Reduced Frequency Limit of Vibrating Airfoils: Part I - Theoretical Analysis
2: (2015)
The Low Reduced Frequency Limit of Vibrating Airfoils. Part II: Numerical Experiments
3: (2015)
The Low Reduced Frequency Limit of Vibrating Airfoils. Part IIIa: Theoretical Quantification of the Unsteady Loading Parameter
4: (2015)
The Low Reduced Frequency Limit of Vibrating Airfoils. Part IIIb: Numerical Quantification of the Unsteady Loading Parameter
8 Ponencia en Congresos
1: (2012)
ASYMPTOTIC DESCRIPTION OF FLUTTER AMPLITUDE SATURATION BY NONLINEAR FRICTION FORCES
2: (2013)
Flutter Amplitude Saturation by Nonlinear Friction Forces: An Asymptotic Approach
3: (2014)
Experimental and Numerical Assessment of the Aeroelastic Stability of Blade Pair Packages
4: (2014)
Flutter Amplitude Saturation by Nonlinear Friction Forces: Reduced Model Validation
5: (2015)
The Low Reduced Frequency Limit of Vibrating Airfoils. Part I: Theoretical Analysis
6: (2015)
The Low Reduced Frequency Limit of Vibrating Airfoils. Part II: Numerical Experiments
7: (2015)
The Low Reduced Frequency Limit of Vibrating Airfoils. Part IIIa: Theoretical Quantification and Influence of Unsteady Loading
8: (2015)
The Low Reduced Frequency Limit of Vibrating Airfoils. Part IIIb: Numerical Quantification and Influence of Unsteady Loading
• TOMA DE DATOS DE MEMORIAS Y CV
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S2i 2017 Observatorio de investigación @ UPM con la colaboración del Consejo Social UPM
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