Receptivity of a supersonic boundary layer over a flat plate. Part 3. Effects of different types of free-stream disturbances

By Yanbao Ma, X. Zhong. Journal of Fluid Mechanics, 2005

144 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Atmospheric Science, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/580a4be729604b811388e0a189f5abc29f8ad630

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. Sanjiva K. Lele
2. Kenneth J. Franko
3. Xiaowen Wang
4. X. Zhong
5. Christophe Bogey
6. Christophe Bailly
7. Yanbao Ma
8. Sergio Pirozzoli

In Atmospheric Science

1. Xiaowen Wang
2. Sanjiva K. Lele
3. Kenneth J. Franko
4. X. Zhong
5. Yanbao Ma

In Computational Mechanics

1. Sanjiva K. Lele
2. Xiaowen Wang
3. Kenneth J. Franko
4. X. Zhong
5. Christophe Bailly
6. Christophe Bogey
7. Yanbao Ma
8. Sergio Pirozzoli

Citations in the corpus

• Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers (2012, background): “Similar to Ma & Zhong (2005), he also found that slow acoustic waves induce much stronger instability waves than fast acoustic waves.”
• Breakdown mechanisms and heat transfer overshoot in hypersonic zero pressure gradient boundary layers (2013, background): “Both first and second mode instabilities may be excited through free stream sound (Ma & Zhong 2005).”