Imperial College London

Dr Rafael Palacios

Faculty of EngineeringDepartment of Aeronautics

Reader in Aeronautics
 
 
 
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Contact

 

+44 (0)20 7594 5075r.palacios CV

 
 
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Location

 

338City and Guilds BuildingSouth Kensington Campus

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Summary

 

Publications

Citation

BibTex format

@inproceedings{González-Salcedo:2017,
author = {González-Salcedo, A and Aparicio-Sanchez, M and Munduate, X and Pires, O and Méndez, B and Palacios, R and Graham, JMR},
title = {A computationally-efficient panel code for unsteady airfoil modelling including dynamic stall},
year = {2017}
}

RIS format (EndNote, RefMan)

TY  - CPAPER
AB - © 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. A new approach based on inviscid panel methods has been developed for airfoils undergoing unsteady kinematics. The model is tailored to practical applications related to wind turbines, taking into account accuracy and computational cost considerations. It is able to represent rigid or deformable airfoils, attached and separated flow focusing also on unsteady cases including dynamic stall. An extensive validation has been carried out including steady and unsteady conditions, while simulations of airfoils with trailing edge flaps have also been performed.
AU - González-Salcedo,A
AU - Aparicio-Sanchez,M
AU - Munduate,X
AU - Pires,O
AU - Méndez,B
AU - Palacios,R
AU - Graham,JMR
PY - 2017///
TI - A computationally-efficient panel code for unsteady airfoil modelling including dynamic stall
ER -