Receptivity of a supersonic boundary layer over a flat plate. Part 1. Wave structures and interactions
By Yanbao Ma, X. Zhong. Journal of Fluid Mechanics, 2003
222 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Atmospheric Science, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/104696ef909a45783d6622d445f3ba4992cd5a25
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
- X. Zhong
- Hermann F. Fasel
- Yanbao Ma
- A. Fedorov
- Dominic von Terzi
- Christian S. J. Mayer
- A. Tumin
- Sanjiva K. Lele
In Atmospheric Science
In Computational Mechanics
- X. Zhong
- Yanbao Ma
- Hermann F. Fasel
- A. Fedorov
- A. Tumin
- Dominic von Terzi
- Christian S. J. Mayer
- Christoph Hader
Citations in the corpus
- 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.”
- Receptivity of a supersonic boundary layer over a flat plate. Part 2. Receptivity to free-stream sound (2003, methodology): “F∗1 and F∗2 are inviscid flux vectors and described in detail in Part 1 (Ma & Zhong 2003).”
- Direct numerical simulation of complete transition to turbulence via oblique breakdown at Mach 3 (2011, methodology): “The phase velocity and αi development in figure 3 show some of the typical behaviour as usually discussed for higher Mach numbers (Ma & Zhong 2003; Tumin 2007).”
- High-Speed Boundary-Layer Instability: Old Terminology and a New Framework (2011, background): “, in [24]) are effectively excited by fast acoustic waves.”