Zobrazeno 1 - 10
of 285
pro vyhledávání: '"Stewart A. L. Glegg"'
Autor:
Máté Szőke, William J. Devenport, Aurélien Borgoltz, W. Nathan Alexander, Nandita Hari, Stewart A. L. Glegg, Ang Li, Rahul Vallabh, Abdel-Fattah M. Seyam
Publikováno v:
AIAA Journal. 60:3651-3660
Autor:
Stewart A. L. Glegg, Máté Szoke, Matthew J. Priddin, William J. Devenport, Nandita Hari, Lorna J. Ayton
Publikováno v:
AIAA AVIATION 2021 FORUM.
The flow field around a series of streamwise rods, referred to as canopies, is investigated using two-dimensional two-component time-resolved particle image velocimetry (PIV) and large eddy simulations (LES) to characterize the changes in the flow fi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8bff0cc317191d1a6ddb47c522e9f2f9
https://dspace.lib.cranfield.ac.uk/handle/1826/17136
https://dspace.lib.cranfield.ac.uk/handle/1826/17136
Autor:
Humza Butt, N. Agastya Balantrapu, Stewart A. L. Glegg, Jarrod T. Banks, Christopher Hickling, William J. Devenport, William N. Alexander
Publikováno v:
AIAA AVIATION 2021 FORUM.
Publikováno v:
AIAA AVIATION 2021 FORUM.
Publikováno v:
AIAA Journal. 57:1899-1913
Measurements and predictions of far-field sound radiated by rounded forward-facing steps immersed in an incompressible turbulent boundary were performed. Four different corner rounding radii equal ...
Publikováno v:
AIAA Journal. 57:1237-1249
Previous studies have demonstrated that structures such as a canopy or finlets placed within a boundary layer over an aerodynamic surface can attenuate pressure fluctuations on the surface without compromising aerodynamic performance. This paper desc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c3836c612192af4ee7b759b2be924523
https://hdl.handle.net/10919/108389
https://hdl.handle.net/10919/108389
Publikováno v:
AIAA AVIATION 2020 FORUM.
Publikováno v:
Journal of Fluid Mechanics. 850:212-245
Aeroacoustic measurements and analysis have been made for an unshrouded rotor partially immersed in a planar equilibrium turbulent boundary layer at low Mach number. This configuration provides an idealized model of inflow distortion effects seen whe