Browsing by Author "Silva, Paulo"
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Item Open Access CODE_MRF.zip(Cranfield University, 2023-10-11 09:00) Silva, Paulo; Tsoutsanis, Panagiotissource codeItem Open Access Data for Paper "Unsteady Multiphase Simulation of Oleo-Pneumatic Shock Absorber Flow"(Cranfield University, 2024-02-21 18:05) Sheikh Al Shabab, Ahmed; Grenko, Bojan; Silva, Paulo; Antoniadis, Antonios; Tsoutsanis, Panagiotis; Skote, MartinDataset for the paper "Unsteady Multiphase Simulation of Oleo-Pneumatic Shock Absorber Flow"Item Open Access Data for the paper A modular multifidelity approach for multiphysics oleo-pneumatic shock absorber simulations(Cranfield University, 2024-02-21 18:42) Sheikh Al Shabab, Ahmed; Silva, Paulo; Grenko, Bojan; Tsoutsanis, Panagiotis; Skote, MartinItem Open Access Data Supporting "A comprehensive CFD investigation of tip vortex trajectory in shrouded wind turbines using compressible RANS solver"(Cranfield University, 2024-03-21 10:43) Silva, PauloThis dataset support the publication "A comprehensive CFD investigation of tip vortex trajectory in shrouded wind turbines using compressible RANS solver" it contains mesh, isosurface and additional dataItem Open Access Data Supporting "Study of Orifice Design on Oleo-Pneumatic Shock Absorber"(Cranfield University, 2024-05-02 11:15) Silva, Paulo; Tsoutsanis, Panagiotis; Skote, Martin; Sheikh Al Shabab, AhmedThis data contain the results of the paper.Item Open Access Data supporting 'Numerical Investigation of full helicopter with and without the ground effect'(Cranfield University, 2022-02-09 18:11) Silva, Paulo; Tsoutsanis, PanagiotisIn the present work, the aerodynamic performance of the full helicopter PSP in hover flight is investigated using a simplified concept of multiple reference frame (MRF) technique in the context of high-order Monotone Upstream Centred Scheme for Conservation Laws (MUSCL) cell-centred finite volume method. The predictions were obtained for two ground distances and several collective pitch angle at tip Mach number of 0.585. The calculations were made for both out-of-ground-effect (OGE) and in-ground-effect (IGE) cases and compared with experimental data in terms of pressure distribution and integrated thrust and torque and vortex system.Item Open Access Mesh PSP robin mod7 - pitch 7deg -OGE(Cranfield University, 2023-12-12 14:48) Silva, PauloThis file is the mesh file for the PSP full helicopter for collective angle 7deg.Item Open Access PSP full helicopter Out ground effect(Cranfield University, 2023-12-12 14:49) Silva, PauloThis data contains results file of the PSP rotor with fuselage for out of ground effect