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Padilla Montero, Ivan ivan.padilla@upm.es

MATEMÁTICA APLICADA A LA INGENIERÍA AEROESPACIAL (DMAIA) / Universidad Politécnica de Madrid

Actividades

Eduction of coherent structures from schlieren images of twin jets using SPOD informed with momentum potential theory in the spectral domain

  • Padilla-Montero, Iván
  • Rodríguez, Daniel
  • Jaunet, Vincent
  • Jordan, Peter

Theoretical And Computational Fluid Dynamics - 20/5/2024

10.1007/s00162-024-00699-w Ver en origen

  • ISSN 09354964

Finite elements and finite volumes methods in wind engineering applications

  • AlSofi, Hosam
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  • Larese, Antonia
  • Padilla, Iván
  • Rossi, Riccardo
  • Scotta, Roberto
  • Wüchner, Roland
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... Ver más Contraer

Advances In Computational Science And Engineering (p. 82-122) - 14/4/2023

10.3934/acse.2023005 Ver en origen

Analysis of the instabilities induced by an isolated roughness element in a laminar high-speed boundary layer

  • Iván Padilla Montero and Fabio Pinna

Journal Of Fluid Mechanics - 25/3/2021

https://doi.org/10.1017/jfm.2021.70 Ver en origen

  • ISSN 00221120

BiGlobal stability analysis of the wake behind an isolated roughness element in hypersonic flow

  • Iván Padilla Montero and Fabio Pinna

Proceedings Of The Institution Of Mechanical Engineers Part G-Journal Of Aerospace Engineering (p. 19) - 1/1/2020

https://doi.org/10.1177/0954410019832733 Ver en origen

  • ISSN 09544100

Este/a investigador/a no tiene libros.

Pressure Measurements at the Mixing-Layer Boundary of Supersonic Twin Jets

  • Iván Padilla-Montero, Daniel Rodríguez, Vincent Jaunet, Stève Girard, Damien Eysseric and Peter Jordan

30/5/2024

https://doi.org/10.2514/6.2024-3147 Ver en origen

Influence of High-Temperature Effects on the Stability of the Wake Behind an Isolated Roughness Element in Hypersonic Flow

  • Iván Padilla Montero, Fernando Miró Miró, Fabio Pinna

31/7/2021

https://doi.org/10.1007/978-3-030-67902-6_55 Ver en origen

Stability Analysis of the Boundary Layer Developing on a Flat Plate with Discrete Roughness Elements in Hypersonic Flow

  • Iván Padilla Montero, Fabio Pinna

7/1/2018

https://doi.org/10.2514/6.2018-1079 Ver en origen

Experimental Validation of PSE Wavepacket Models for Supersonic Twin Jets Using Schlieren Imaging and Potential-Momentum-Theory-Based SPOD

  • Iván Padilla-Montero, Daniel Rodriguez, Vincent Jaunet and Peter Jordan

30th Aiaa/Ceas Aeroacoustics Conference (2024) - 31/5/2024

10.2514/6.2024-3146 Ver en origen

Mean Flow and Linear Stability Analysis of Twin Supersonic Jets

  • Padilla Montero, Ivan
  • Rodriguez, Daniel
  • Jaunet, Vincent
  • Girard, Steve
  • Eysseric, Damien
  • Jordan, Peter

Aiaa Aviation 2023 Forum - 8/6/2023

10.2514/6.2023-3350 Ver en origen

INVESTIGATION OF COHERENT MOTIONS AND NOISE RADIATION IN TWIN SUPERSONIC JETS USING HIGH-SPEED SCHLIEREN IMAGES

  • Padilla-Montero I
  • Rodríguez D
  • Jaunet V
  • Girard S
  • Eysseric D
  • Jordan P

Proceedings Of Forum Acusticum - 1/1/2023

  • ISSN 22213767
  • iMarina

Analysis of the boundary layer stability to assess flow separation control capability in low-pressure turbines

  • Iván Padilla, Jorge Saavedra, Guillermo Paniagua, Fabio Pinna

Proceedings Of The 6th European Conference On Computational Mechanics: Solids, Structures And Coupled Problems, Eccm 2018 And 7th European Conference On Computational Fluid Dynamics, Ecfd 2018 - 14/6/2018

  • iMarina

Este/a investigador/a no tiene documentos de trabajo.

Este/a investigador/a no tiene informes técnicos.

Short-time analysis of large-scale structures in unsteady flows

  • PADILLA MONTERO, IVAN (Participante)
  • RODRIGUEZ ALVAREZ, Daniel (Investigador principal (IP))

Ejecución: 01-09-2023 - 28-02-2026

Tipo: Internacional

Importe financiado: 206641,20 Euros.

  • iMarina

Este/a investigador/a no tiene tesis dirigidas.

Este/a investigador/a no tiene patentes o licencias de software.

Última actualización de los datos: 28/08/24 13:48