Results 41 to 50 of about 150,010 (213)

Broadband Noise Reduction of a Two-Stage Fan with Wavy Trailing-Edge Blades

open access: yesAerospace
In this paper, a numerical investigation is performed to study the broadband noise of a fan stage with wavy trailing-edge blades. A study of the wavelength and ratio of amplitude to wavelength (H/L) is conducted to better understand the noise reduction ...
Ruibiao Gao   +4 more
doaj   +1 more source

A Study of the Dependence of the Mach Stem Height on the Trailing Edge Height

open access: yesFluids, 2021
The Mach stem height is an important parameter in the Mach reflection of steady supersonic flow. Various experimental, numerical, and theoretical works have been conducted to study this parameter in the past. However, much of the established work focuses
Chen-Yuan Bai, Zi-Niu Wu
doaj   +1 more source

Influence of Gurney Flap and Leading-Edge/Trailing-Edge Flaps on the Stall Characteristics and Aeroacoustic Performance of Airfoils

open access: yesFluids
In aerospace, flow control techniques have improved the separation flow characteristics around airfoils by various means. In this paper, the delayed detached eddy simulation (DDES) technique is used to simulate the detailed flow field around the NACA0021
Zelin Liu, Kaidi Li, Xiaojing Sun
doaj   +1 more source

Computation of Trailing Edge Noise with a Discontinuous Galerkin Method [PDF]

open access: yes, 2010
Trailing edge noise of a semi-infinite, thin, flat plate situated in low Mach number flow is computed in two spatial dimensions. The Acoustic Perturbation Equations (APE), which are employed as governing equations, are discretized via a Discontinuous ...
Bauer, Marcus
core   +1 more source

Aerodynamic noise from rigid trailing edges with finite porous extensions

open access: yes, 2017
This paper investigates the effects of finite flat porous extensions to semi-infinite impermeable flat plates in an attempt to control trailing-edge noise through bio-inspired adaptations.
Ayton, L. J., Kisil, A. V.
core   +1 more source

Computer-Aided Simulations of Convective Heat Transfer in a Wedged Channel with Pin-Fins at Various Outlet Arrangements and Nonuniform Diameters

open access: yesAdvances in Mechanical Engineering, 2013
The turbine blade works at high thermal loads, especially the trailing edge of the blade due to the hot gas leakage flow. Pin-fins are well recognized as a kind of effective device to augment the convective heat transfer and effectively cool the trailing
Qitao Zhou   +4 more
doaj   +1 more source

Solitonic asymptotics for the Korteweg-de Vries equation in the small dispersion limit

open access: yes, 2009
We study the small dispersion limit for the Korteweg-de Vries (KdV) equation $u_t+6uu_x+\epsilon^{2}u_{xxx}=0$ in a critical scaling regime where $x$ approaches the trailing edge of the region where the KdV solution shows oscillatory behavior.
Claeys T.   +7 more
core   +1 more source

Study on effect of some geometric transformations of the trailing edge of airfoils on their aerodynamic parameters

open access: yesAdvanced Engineering Research, 2016
The work objective is to evaluate how the geometric transformations of the trailing edge of some airfoils affect the aerodynamic characteristics. Such transformations as the trailing edge thickening and rounding are considered.
Konstantin I. Mescheryakov   +1 more
doaj   +1 more source

Eigenvalues in trailing edge flows [PDF]

open access: yesJournal of the Australian Mathematical Society, 1975
Abstract A wake similarity solution for symmetric uniform shear flows merging at the trailing edge of a flat plate has associated with it an eigenfunction problem which was overlooked by Hakkinen and O'Neil (1967). An asymptotic formula for large eigenvalues is obtained and compared with another such formula related to both the Goldstein (1930) inner ...
openaire   +2 more sources

Aerodynamic behavior of an airfoil with morphing trailing edge for wind turbine applications [PDF]

open access: yes, 2014
The length of wind turbine rotor blades has been increased during the last decades. Higher stresses arise especially at the blade root because of the longer lever arm.
Ernst, Benedikt   +2 more
core   +2 more sources

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