Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Jorge Aguilar-Cabello"'
Publikováno v:
SoftwareX, Vol 20, Iss , Pp 101256- (2022)
We present a translation of the original Matlab DPIVSoft code to a complete open source code implemented in Python, to perform Particle Image Velocimetry (PIV) in two-dimensions, in parallel, and with interrogation window shifting along with the doub
Externí odkaz:
https://doaj.org/article/82a641e44a7d466b82610025580d14ca
Publikováno v:
CEAS Aeronautical Journal
CEAS Aeronautical Journal, 2022, 13, pp.97-112. ⟨10.1007/s13272-021-00555-1⟩
CEAS Aeronautical Journal, Springer, 2021, ⟨10.1007/s13272-021-00555-1⟩
CEAS Aeronautical Journal 13, 97-112 (2022). doi:10.1007/s13272-021-00555-1
CEAS Aeronautical Journal, 2022, 13, pp.97-112. ⟨10.1007/s13272-021-00555-1⟩
CEAS Aeronautical Journal, Springer, 2021, ⟨10.1007/s13272-021-00555-1⟩
CEAS Aeronautical Journal 13, 97-112 (2022). doi:10.1007/s13272-021-00555-1
CEAS Aeronautical Journal 13, 97-112 (2022). doi:10.1007/s13272-021-00555-1
Published by Springer, Wien [u.a.]
Published by Springer, Wien [u.a.]
Autor:
Manuel Garrido-Martin, Tobias Bölle, Jorge Aguilar-Cabello, J.HERMENEGILDO GARCIA-ORTIZ, Carlos Del Pino, Paloma Gutierrez Castillo
The decay of trailing vortices is a fundamental problem in fluid mechanics and constitutes the basis of control applications that intend to alleviate the wake hazard. In order to progress, we use the recently developed modal-decomposition technique t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::768cf63ea337d20986af754eece59448
https://doi.org/10.1063/5.0117611
https://doi.org/10.1063/5.0117611
Autor:
Paloma Guitérrez-Castillo, Antonio J. Hijano-Reyes, Jorge Aguilar-Cabello, Carlos del Pino, J.J. Serrano-Aguilera, Francisco J. Blanco-Rodríguez, L. Parras, Maria Isabel Olmo-Sanchez
Publikováno v:
ICERI2021 Proceedings.
Autor:
Carlos del Pino, Luis Parras, Jorge Aguilar-Cabello, Paloma Gutierrez-Castillo, Sergio Alcalde-Morales
Publikováno v:
Journal of Wind Engineering and Industrial Aerodynamics. 208:104459
The lift coefficient for a flat plate at low angles of attack is obtained experimentally for various aspect ratios (AR = 1, 2, 4, 8) and moderate Reynolds numbers (Re = 40 × 103 to Re = 200 × 103). The variation of the
Autor:
Luis Parras, Jorge Aguilar-Cabello, Paloma Gutierrez-Castillo, Carlos del Pino, Enrique Sanmiguel-Rojas
Publikováno v:
Physics of Fluids. 32:055107
The variation of the lift coefficient in a symmetric airfoil (NACA 0012 profile) at very small angles of attack is studied experimentally and numerically for a range of low chord-based Reynolds numbers, Re. Experimentally, the non-linearity around th