International audienceFive temporally-developing isothermal round jets at a diameter-based Reynolds number ReD of 3,125 and Mach numbers M of 0.3, 0.6, 0.9, 1.3 and 2 have been computed using direct numerical simulation. The flow and near acoustic fields of the jets are described in detail, and cross-correlations between the two fields are presented in order to identify noise generation mechanisms, and especially that associated with the jet potential-core closing. That closing is found to occur later at a higher Mach number. Apart from that, the jet flow properties, including velocity spectra, are similar, and even nearly identical for M ≤ 1.3. The jets appear to radiate acoustic waves mainly in the downstream direction, with amplitude inc...
We present experimental results for the acoustic field of jets in the Mach number range 0.35 ≤ M ≤ 0...
This work presents advances towards a linear surface-based model for the jet noise source in simple ...
Noise sources in high-speed jets were identified by directly correlating flow density fluctuation (c...
International audienceTwo temporally developing isothermal round jets at a Mach number of 0.9 and Re...
International audienceIn the present study, two-dimensional spatial correlations are calculated in t...
International audienceIn a previous work [Bogey, J. Fluid Mech. 859, 1022 (2019)], the potential-cor...
A temporally-developing supersonic round jet at a Mach number of 2 and at a diameter-based Reynolds ...
An acoustic field generated by subsonic jets at low Reynolds numbers was investigated. This work is ...
Round jets having a Mach number of 0.9 and a Reynolds number of 1700 are computed by di...
In this paper we present the experimental results of a detailed investigation of the flow and acoust...
Jet noise is an extensively studied phenomenon since the deployment of the first civil jet aircraft ...
We study the velocity field of unforced, high Reynolds number, subsonic jets, issuing from round noz...
International audienceThe acoustic field generated by the synchronized vortex street in self-excited...
Both aerodynamic and near field acoustic behavior of several unheated axisymmetric shock free and sh...
A wave-packet ansatz is used to model noise generation by organized, large-scale structures. The spe...
We present experimental results for the acoustic field of jets in the Mach number range 0.35 ≤ M ≤ 0...
This work presents advances towards a linear surface-based model for the jet noise source in simple ...
Noise sources in high-speed jets were identified by directly correlating flow density fluctuation (c...
International audienceTwo temporally developing isothermal round jets at a Mach number of 0.9 and Re...
International audienceIn the present study, two-dimensional spatial correlations are calculated in t...
International audienceIn a previous work [Bogey, J. Fluid Mech. 859, 1022 (2019)], the potential-cor...
A temporally-developing supersonic round jet at a Mach number of 2 and at a diameter-based Reynolds ...
An acoustic field generated by subsonic jets at low Reynolds numbers was investigated. This work is ...
Round jets having a Mach number of 0.9 and a Reynolds number of 1700 are computed by di...
In this paper we present the experimental results of a detailed investigation of the flow and acoust...
Jet noise is an extensively studied phenomenon since the deployment of the first civil jet aircraft ...
We study the velocity field of unforced, high Reynolds number, subsonic jets, issuing from round noz...
International audienceThe acoustic field generated by the synchronized vortex street in self-excited...
Both aerodynamic and near field acoustic behavior of several unheated axisymmetric shock free and sh...
A wave-packet ansatz is used to model noise generation by organized, large-scale structures. The spe...
We present experimental results for the acoustic field of jets in the Mach number range 0.35 ≤ M ≤ 0...
This work presents advances towards a linear surface-based model for the jet noise source in simple ...
Noise sources in high-speed jets were identified by directly correlating flow density fluctuation (c...