Zobrazeno 1 - 10
of 167
pro vyhledávání: '"James D. Baeder"'
Publikováno v:
Wind Energy, Vol 27, Iss 9, Pp 900-921 (2024)
Abstract The performance of a wind turbine and its efficiency majorly depends on wind‐to‐rotor efficiency. The aerodynamic design of the wind turbine blades using high‐fidelity tools such as adjoint‐computational fluid dynamics (CFD) is accur
Externí odkaz:
https://doaj.org/article/0f2e8927d849454b8d82ce3bcb5ab294
Publikováno v:
AIAA Journal. 61:2552-2569
This work illustrates the use of artificial neural network modeling to study and characterize broadband blade-wake interaction noise from hovering small unmanned aerial systems rotors subject to varying airfoil geometries, rotor geometries, and opera
Publikováno v:
Journal of the American Helicopter Society. 68:1-17
Experimental near-wake flow field measurements from two Penn State University water tunnel tests of a defeatured helicopter hub are compared with two unsteady computational fluid dynamics (CFD) analyses: CREATETM-AV Helios and the University of Maryl
Publikováno v:
AIAA Journal. 60:1549-1564
This study presents numerical findings of the response of a flat plate to transverse, sharp-edged gusts at a low Reynolds number (Re=40,000). A split velocity method was implemented in a three-dime...
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
Journal of the American Helicopter Society. 66:1-17
Recently, an asymmetric lift-offset compound helicopter has been conceptualized at the University of Maryland with the objective of improving the overall performance of a medium-lift utility helicopter. The investigated form of lift-compounding incor
Publikováno v:
AIAA Journal. 59:49-64
The split velocity method was applied to study the response of a finite flat-plate wing with an aspect ratio of four encountering a large transverse gust with various gust widths. The gust is model...
Publikováno v:
Journal of the American Helicopter Society. 65:1-14
To expand the cruise speed of a compound helicopter, alleviating the compressibility effects on the advancing side with reduced rotor RPM is proved to be an effective design feature, which results in high advance ratio flight regime. To investigate t
Publikováno v:
International Journal of Computational Fluid Dynamics. 34:61-74
The multi-mesh, multi-solver paradigm makes use of multiple Computational Fluid Dynamics (CFD) solvers in a single overset framework. A framework-level implementation of the Generalised Minimal Res...
Autor:
Jingcheng Lu, James D. Baeder
Publikováno v:
AIAA SCITECH 2022 Forum.