Receptivity of a supersonic boundary layer over a flat plate. Part 2. Receptivity to free-stream sound

By Yanbao Ma, X. Zhong. Journal of Fluid Mechanics, 2003

163 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Atmospheric Science, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/196da5e6bdc377b3f796a0e91d2c9c89cd8e554a

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. X. Zhong
2. Yanbao Ma
3. A. Fedorov
4. A. Tumin

In Atmospheric Science

1. X. Zhong
2. Yanbao Ma
3. A. Fedorov
4. A. Tumin

In Computational Mechanics

1. X. Zhong
2. Yanbao Ma
3. A. Fedorov
4. A. Tumin
5. Xiaowen Wang
6. S. Schneider
7. Hermann F. Fasel

Citations in the corpus

• High-Speed Boundary-Layer Instability: Old Terminology and a New Framework (2011, background): “Ma and Zhong [24,25] showed that the fast modesF 1 ,F 2 , etc.”
• Receptivity of a supersonic boundary layer over a flat plate. Part 1. Wave structures and interactions (2003, background): “In part 2 (Ma & Zhong 2003), the receptivity mechanisms of a supersonic boundary layer to free-stream sound will be investigated.”
• Receptivity of a supersonic boundary layer over a flat plate. Part 3. Effects of different types of free-stream disturbances (2005, methodology): “As discussed in Ma & Zhong (2003b), the dominant boundary-layer disturbances in receptivity to free-stream fast acoustic waves are mode I waves, which are always stable and convert to the second-mode waves.”