We study both, by experimental and numerical means the fluid dynamical phenomenon of so-called edge tones. Of particular interest is the clarification of certain scaling laws relating the frequency ƒ to geometrical quantities, namely 푑, the height of the jet, 푤, the stand-off distance and the velocity of the jet. We conclude that the Strouhal number S푑 is given by S푑 = C · (푑/푤)푛 with 푛 ≈ 1 in our case. Moreover, the constant C of the experiment agrees within 10-15% with the result of the simulation. As for the frequency dependence on the geometry and on the jet velocity there is a very good agreement of experimental and numerical results
For the case of a jet originating from a fully turbulent channel flow and impinging upon a sharp edg...
The production of self-sustained tones (up to 125 dB) by a low Mach number free plane jet impinging...
High intensity acoustic radiation occurs when turbulence convects past airframe trailing edges. A ma...
We study both, by experimental and numerical means the fluid dynamical phenomenon of edge tones. Of ...
This paper is the first half of a two-part publication. In these papers the well-known low Mach numb...
This paper is the second half of a two-part publication. The first part containsa detailed overview ...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
P(論文)An edge tone is self excited sound, which is one of the important phenomena in subsonic aerodyn...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
The noise emission generated by the passage of a turbulent airstream over the trailing edge of a sem...
We show the effect of correcting the acoustic spectrum formula for a high speed jet interacting with...
International audienceThe impingement of a round jet issued from a convergent nozzle is known to pro...
An investigation of the instability frequency was undertaken. Measurements revealed that the hot wir...
The source of audible tones occurring with a coaxial nozzle in a range of low Mach numbers is explor...
The growth in amplitude of a sinuous disturbance propagating along a fully turbulent diverging plan...
For the case of a jet originating from a fully turbulent channel flow and impinging upon a sharp edg...
The production of self-sustained tones (up to 125 dB) by a low Mach number free plane jet impinging...
High intensity acoustic radiation occurs when turbulence convects past airframe trailing edges. A ma...
We study both, by experimental and numerical means the fluid dynamical phenomenon of edge tones. Of ...
This paper is the first half of a two-part publication. In these papers the well-known low Mach numb...
This paper is the second half of a two-part publication. The first part containsa detailed overview ...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
P(論文)An edge tone is self excited sound, which is one of the important phenomena in subsonic aerodyn...
Motivated by the problem of jet–flap interaction noise, we study the tonal dynamics that occurs when...
The noise emission generated by the passage of a turbulent airstream over the trailing edge of a sem...
We show the effect of correcting the acoustic spectrum formula for a high speed jet interacting with...
International audienceThe impingement of a round jet issued from a convergent nozzle is known to pro...
An investigation of the instability frequency was undertaken. Measurements revealed that the hot wir...
The source of audible tones occurring with a coaxial nozzle in a range of low Mach numbers is explor...
The growth in amplitude of a sinuous disturbance propagating along a fully turbulent diverging plan...
For the case of a jet originating from a fully turbulent channel flow and impinging upon a sharp edg...
The production of self-sustained tones (up to 125 dB) by a low Mach number free plane jet impinging...
High intensity acoustic radiation occurs when turbulence convects past airframe trailing edges. A ma...