Zobrazeno 1 - 10
of 46
pro vyhledávání: '"Michael Strelets"'
Publikováno v:
AIAA Journal. 60:2441-2457
This study investigates the instabilities of the interstage flow between a rotor and a stator in turbomachinery and evaluates their impact on the fan noise. By viewing the interstage flow as the so...
Publikováno v:
AIAA Journal. :1-7
Global instability analysis is used to investigate the effects of extended regions of laminar flow on both unswept and swept infinite-span wings. The formulation is based on the Reynolds-averaged N...
Publikováno v:
AIAA Journal. :1-17
This paper presents two enhancements of the efficient broadband time-domain impedance model proposed by Dragna, Pineau, and Blanc-Benon in 2015. It treats lined walls in the framework of the macros...
Publikováno v:
AIAA Journal. 57:5168-5181
The fan broadband noise of a rotor–stator system representing a turbofan aeroengine is investigated using the improved delayed detached-eddy-simulation approach. The baseline configuration of the N...
Publikováno v:
AIAA AVIATION 2021 FORUM.
Publikováno v:
Journal of Fluid Mechanics. 881:3-22
Global stability analysis is used to analyse the onset of transonic buffet on infinite swept and unswept wings. This high-Reynolds-number flow is governed by the unsteady Reynolds averaged Navier–Stokes equations. The analysis generalizes earlier s
Publikováno v:
Journal of Fluid Mechanics. 901
Publikováno v:
AIAA AVIATION 2020 FORUM.
Publikováno v:
AIAA Journal. 56:2283-2297
The Paper presents the aerodynamic and turbulent aspects of a project devoted to creating and validating a high-fidelity computational-fluid-dynamics-based system for the prediction of the performa...
Publikováno v:
Journal of Sound and Vibration. 411:328-345
A numerical method for aeroacoustic source characterization of in-duct components at frequencies beyond the cut-on frequencies of several acoustic modes is presented. Assuming linearity and time invariance, any ducted component can be fully character