We study both, by experimental and numerical means the fluid dynamical phenomenon of edge tones. Of particular interest is the verification of scaling laws relating the frequency $f$ to given quantities, namely $d$, the height of the jet, $w$, the stand–off distance and the velocity of the jet. We conclude that the Strouhal number $S_d$ is related to the geometrical quantities through $S_d = C ⋅ (d / w)^n$ with $n \approx 1$, in contrast to some analytical treatments of the problem. The constant $C$ of the experiment agrees within 13–15% with the result of the numerical treatment. Only a weak dependence on the Reynolds number with respect to d is observed. In general, a very good agreement of the experimental and the numerical simulations i...
The performance of active feedback control of edge tone phenomenon by the control flow is investigat...
The main objective of the present work is to investigate the mechanism of trailing-edge airfoil nois...
The present work investigates the broadband noise reduction that can be achieved using trailing-edge...
We study both, by experimental and numerical means the fluid dynamical phenomenon of so-called edge ...
P(論文)An edge tone is self excited sound, which is one of the important phenomena in subsonic aerodyn...
This paper is the second half of a two-part publication. The first part containsa detailed overview ...
This paper is the first half of a two-part publication. In these papers the well-known low Mach numb...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
The production of self-sustained tones (up to 125 dB) by a low Mach number free plane jet impinging...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
For the case of a jet originating from a fully turbulent channel flow and impinging upon a sharp edg...
The nature of the instability governing the self-sustained tones produced by a low Mach number free ...
The design of aircraft propulsion configurations must digress from the typical configurations that a...
International audienceCascade broadband trailing-edge noise is investigated experimentaly in an aera...
This paper presents experimental data concerning the flow and noise generated by a sharp-edged flat ...
The performance of active feedback control of edge tone phenomenon by the control flow is investigat...
The main objective of the present work is to investigate the mechanism of trailing-edge airfoil nois...
The present work investigates the broadband noise reduction that can be achieved using trailing-edge...
We study both, by experimental and numerical means the fluid dynamical phenomenon of so-called edge ...
P(論文)An edge tone is self excited sound, which is one of the important phenomena in subsonic aerodyn...
This paper is the second half of a two-part publication. The first part containsa detailed overview ...
This paper is the first half of a two-part publication. In these papers the well-known low Mach numb...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
The production of self-sustained tones (up to 125 dB) by a low Mach number free plane jet impinging...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
For the case of a jet originating from a fully turbulent channel flow and impinging upon a sharp edg...
The nature of the instability governing the self-sustained tones produced by a low Mach number free ...
The design of aircraft propulsion configurations must digress from the typical configurations that a...
International audienceCascade broadband trailing-edge noise is investigated experimentaly in an aera...
This paper presents experimental data concerning the flow and noise generated by a sharp-edged flat ...
The performance of active feedback control of edge tone phenomenon by the control flow is investigat...
The main objective of the present work is to investigate the mechanism of trailing-edge airfoil nois...
The present work investigates the broadband noise reduction that can be achieved using trailing-edge...