Excitation and evolution of radiating modes in supersonic boundary layers. II: Back effect of spontaneously radiated Mach waves
From MaRDI portal
Publication:6496938
DOI10.1017/JFM.2024.277MaRDI QIDQ6496938
Publication date: 6 May 2024
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Cites Work
- Unnamed Item
- On generation of sound in wall-bounded shear flows: back action of sound and global acoustic coupling
- Triple-deck analysis of transonic high Reynolds number flow through slender channels
- On the role of acoustic feedback in boundary-layer instability
- Stability and receptivity characteristics of a laminar separation bubble on an aerofoil
- ON THE STABILITY OF THE DEVELOPING FLOW IN A CHANNEL OR CIRCULAR PIPE
- On the first-mode instability in subsonic, supersonic or hypersonic boundary layers
- Experiments on stability and transition at Mach 3
- Mach wave radiation of nonlinearly evolving supersonic instability modes in shear layers
- Prediction of installed jet noise
- Numerical investigation of the tone noise mechanism over laminar airfoils
- Nonlinear evolution of subsonic and supersonic disturbances on a compressible free shear layer
This page was built for publication: Excitation and evolution of radiating modes in supersonic boundary layers. II: Back effect of spontaneously radiated Mach waves