[PDF] Top 20 Non viscous sensitivity analysis of noise generation mechanism in a low Mach number jet
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Non viscous sensitivity analysis of noise generation mechanism in a low Mach number jet
... kind of ’energy’ ...r in the following. Sensitivity coefficients can be therefore explained as how the response of any variation in the output of a system expressed as ... Voir le document complet
10
Non viscous sensitivity analysis of noise generation mechanism in a low Mach number jet
... step of the sensitivity analysis of some quadratic quantity related to acoustic waves with respect to any flow or wall disturbance is proposed in the configuration of subsonic ... Voir le document complet
11
Estimation of whistling of an orifice in a reverberating duct at low Mach number
... sible of pure tone noise generation by an orifice in confined ...on low Mach number such that the fluid compressibility inside the orifice does not play a ... Voir le document complet
7
Sensitivity analysis for subsonic jet using adjoint of non local stability equations
... Introduction In the past many investigators 1–6 have suggested based to theoretical and experimental results that flow instabilities is the dominant noise-generation mechanism for jet ... Voir le document complet
13
PSE-based sensitivity analysis of turbulent and supersonic single stream jet
... waves of the ...mixing noise from supersonic jets. In this work assuming that the large-scale structures can be modelled as the flow field generated by the evolution of instability waves ... Voir le document complet
14
PSE-based sensitivity analysis of turbulent and supersonic single stream jet
... Reducing noise emission from jet is a major topics of ...structures of a turbulent single-stream jet, which are parts of the noise generation ... Voir le document complet
15
Sensitivity analysis of likelihood ratio test in K distributed and/or Gaussian noise
... Terms—Detector sensitivity, distributed noise, likeli- hood ratio, radar ...ETECTION of a target in competition with strong clutter and thermal noise is a predominant ... Voir le document complet
6
Design of a shock tube for jet noise research
... Initial Shock Tube Conditions -Shock - - Interface - Expansion Pressure After Diaphragm Breaks Jet Reflected Shock Pressure After Shock Reflection.. Figure 2-1: Schematic of wave sys[r] ... Voir le document complet
132
Accounting for convective effects in zero-Mach-number thermoacoustic models
... Introduction In reacting flows, the unsteady heat release rate is a source of acoustic-pressure fluctuations [1] ...conditions, a constructive coupling between combustion and acoustics can ... Voir le document complet
18
Analysis and Optimization of Noise Response for Low-Noise CMOS Image Sensors
... shows a microphotography of the test image sensor ...Photography of the test image sensor Noise measurements were done in order to evaluate impacts of dark current minimization ... Voir le document complet
5
Application of the compressible and low-mach number approaches to large-eddy simulation of turbulent flows in aero-engines
... becomes a more and more demanded tool to improve the design of ...next generation low-emission engines at the industrial development level and the ability for LES to provide information on the ... Voir le document complet
180
Sensitivity Analysis and Uncertainty Quantification of Plasma Jet Instabilities in the VKI Plasmatron
... investigated. In this case, the input would be an uncertain function of temperature and/or pressure a bounds should be put on the ...properties. A similar methodology of stochastic col- ... Voir le document complet
111
Cost-benefit analysis of ultra-low sulfur jet fuel
... For example, the global GEOS-Chem inventory for the run used to create the CMAQ full aviation ULS scenario boundary conditions contained full aviation emissions with a[r] ... Voir le document complet
122
Global Sensitivity Analysis: a new generation of mighty estimators based on rank statistics
... as a screening me- chanics for the DAE system given by (23) and ...Conclusion In this paper, we explain how to use the estimator proposed by Chatterjee in [ 9 ] to provide a very nice and ... Voir le document complet
39
Accounting for convective effects in zero-Mach-number thermoacoustic models
... Introduction In reacting flows, the unsteady heat release rate is a source of acoustic-pressure fluctuations [1] ...conditions, a constructive coupling between combustion and acoustics can ... Voir le document complet
19
Volume charge carrier number fluctuations probed by low frequency noise measurements in InN layers
... showed a clear linear dependence. The energy level of the trap was deduced from the slope of the linear fit, its energy position being around 52 meV below the conduction band ...As a ... Voir le document complet
4
Optipris : A constant pressure air intake for a Mach number up to 0.3
... determined. A design law is obtained from which it is possible to define a constant pres- sure air intake for given flow rates and pressure ...for a range of pressure coefficients from 0 to ... Voir le document complet
3
Matrix Generation in Isogeometric Analysis by Low Rank Tensor Approximation
... Mathematics in the Sciences, Leipzig, Germany ...task of matrix assembly in Isogeometric Analysis (IGA) is more challenging than in the case of tra- ditional finite element ... Voir le document complet
20
Study of a low Mach nuclear core model for single-phase flows
... means of the method of characteristics even if the success of this method applied to the Lmnc model relies heavily on the one-dimensional ...extension of the MOC scheme to 2D will be ... Voir le document complet
18
Adjoint-based acoustic wave sensitivity of a double-stream jet
... references in various part of the present work and beyond ! Receptivity, sensitivity (incompressible, compressible ) , resolvent: Hill (1995), Airiau(1999), Cervino & Bewley (2003), Spagnoli ... Voir le document complet
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