Experimental aeroacoustics study on jet noise reduction using tangential air injection
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- Type
- dissertation
- Published
- 2011-01-01
- Cited by
- 5
- References
- 81
- OpenAlex
- https://openalex.org/W22069141
- Semantic Scholar
- https://api.semanticscholar.org/CorpusID:108218457
Keywords
Aeroacoustics, Computational aeroacoustics, Jet (fluid), Noise reduction, Jet noise
References
- Supersonic Jet Noise and its Reduction Using Microjet Injection
- Computations of Nonlinear Propagation of Sound Emitted from High Speed Mixing Layers
- Atmospheric absorption of high frequency noise and application to fractional-octave bands
- Turbulent mixing noise from supersonic jets
- Acoustic and flow fields of an excited high Reynolds number axisymmetric supersonic jet
- Sound radiation due to unsteady dissipation in turbulent flows
- A review of jet mixing enhancement for aircraft propulsion applications
- Nozzle Shaping for Reduction of Jet Noise from Single Jets
- On the Two Components of Turbulent Mixing Noise from Supersonic Jets
- Experimental Study of the Far Field of Incompressible Swirling Jets
- Efficient detection of spurious vectors in particle image velocimetry data
- Development and evaluation of a 3-D microphone array to locate individual acoustic sources in a high-speed jet
- Tracer particles and seeding for particle image velocimetry
- Turbulence and noise suppression of a high-speed jet by water injection
- Basic principles of aerodynamic noise generation
- Influence of Nozzle Geometry on the Noise of High-Speed Jets
- Use of High-Speed Microjets for Active Separation Control in Diffusers
- Subsonic jet aeroacoustics: associating experiment, modelling and simulation
- Jet Mixing Noise from Fine-Scale Turbulence
- Investigation of Noise Source Mechanisms in Subsonic Jets
Cited by
- Novel Approach for Industrial Noise Cancellation in Speech Using ICA-EMD with PSO
- Aero-acoustic Characteristics of Compressible Jets from Chevron Nozzle
- Jet noise reduction using co-axial swirl flow with curved vanes
- Effect of chevron nozzle penetration on aero-acoustic characteristics of jet at M = 0.8
- Correlation in the Near and Far Field of Compressible Jet to Identify Noise Source Characteristics
Related papers
- Reductions in Multi-Component Jet Noise by Water Injection
- Aeroacoustics investigation of the noise from an asymmetric nozzle
- The simulation of flight effects on jet noise using co-flowing airstreams
- Aeroacoustics of axisymmetric single and dual flow exhaust nozzles
- Computational Study of the Effect of Slotted Air Injection on Jet Noise
- The theoretical modelling of aerodynamic noise
- High-fidelity Simulation of Jet Noise from Rectangular Nozzles . [Large Eddy Simulation (LES) Model for Noise Reduction in Advanced Jet Engines and Automobiles]