Aero-Acoustic Performance of a Tube With Forward-Slanted Oblique Perforations for Reducing the Noise of a Supersonic Jet

The International Journal of Acoustics and Vibration
doi 10.20855/ijav.2004.9.1154
Full Text
Abstract

Available in full text

Date
Authors
Publisher

International Institute of Acoustics and Vibration (IIAV)

Related search

Characterization of Supersonic Laboratory-Scale Jet Noise With Vector Acoustic Intensity

2017English

Using RANS to Predict the Performance of Mixers in Reducing Jet Noise

2004English

Supersonic Jet Noise: Main Sources and Reduction Methodologies

Journal of Engineering Science and Technology Review
Engineering
2014English

Experiments With a Supersonic Tube Wind-Tunnel

1970English

Visualization of Supersonic Jet Noise Using Schlieren Method and Abel Inversion

Journal of the Visualization Society of Japan
2008English

A Model Supersonic Buried-Nozzle Jet: Instability and Acoustic Wave Scattering and the Far-Field Sound

Journal of Fluid Mechanics
Mechanics of MaterialsCondensed Matter PhysicsMechanical Engineering
2015English

Unified Aerodynamic-Acoustic Formulation for Aero-Acoustic Structure Coupling

Journal of Mechanics Engineering and Automation
2013English

On the Scaling Laws and Similarity Spectra for Jet Noise in Subsonic and Supersonic Flow

The International Journal of Acoustics and Vibration
2008English

Flow Visualization of Two-Dimensional Secondary Jet Interaction With a Supersonic Flow

Journal of the Visualization Society of Japan
1990English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy