Mach number distribution for subsonic flow over a bump.
![Mach number distribution for subsonic flow over a bump.](https://www.researchgate.net/publication/316891459/figure/fig2/AS:494361240899584@1494876312576/Mach-number-distribution-for-subsonic-flow-over-a-bump.png)
![](http://www.propfan.net/PIX/2DE/channel_mconv_cmp_600.jpg)
2DE: 2D Euler CFD tool
![](https://media.springernature.com/m685/springer-static/image/art%3A10.1186%2Fs42774-022-00119-9/MediaObjects/42774_2022_119_Fig4_HTML.png)
Survey of control techniques to alleviate repercussions of shock-wave and boundary-layer interactions, Advances in Aerodynamics
![](https://www.researchgate.net/publication/308852434/figure/fig6/AS:668879500091411@1536484708882/Sailwing-construction-concept-from-9_Q320.jpg)
of radiative and convective heat transfer per unit length of radiant
What is the mach number in a supersonic flight? - Quora
![](https://static.cambridge.org/content/id/urn%3Acambridge.org%3Aid%3Aarticle%3AS0022112021003128/resource/name/S0022112021003128_figAb.png?pub-status=live)
Direct numerical simulation of a turbulent boundary layer over a bump with strong pressure gradients, Journal of Fluid Mechanics
![](https://ascelibrary.com/cms/10.1061/(ASCE)AS.1943-5525.0001166/asset/86f3937c-d7e8-4d5a-a63b-f3c42f23508b/assets/images/large/figure13.jpg)
Design of Supercritical Low-Reynolds-Number Airfoils for Fixed-Wing Flight on Mars, Journal of Aerospace Engineering
![](https://www.researchgate.net/publication/369521614/figure/fig1/AS:11431281130149166@1679758584370/Bow-wave-elevation-a-F0-b-F014-c-F0225-d-F024_Q320.jpg)
Snapshot of the argon bubble (d = 0.5 mm) distribution in the symmetry
![](https://www.researchgate.net/publication/252601190/figure/fig5/AS:298169205313538@1448100486132/a-Physical-situation-for-the-flow-over-a-circular-arc-bump-b-Mach-contours-for.png)
a ) Physical situation for the flow over a circular arc bump; ( b )
![](https://www.iag.uni-stuttgart.de/dateien/img/luftfahrzeugaero/INAFLOWT2.png?__scale=w:1000,h:1000,q:100,t:3)
Research, Institute of Aerodynamics and Gas Dynamics
![](https://www.researchgate.net/profile/Benjamin-Uekermann/publication/321289778/figure/tbl1/AS:667766025621529@1536219235929/gives-a-first-overview_Q320.jpg)
Pressure distribution over the test turbine blade, comparison with
![](https://www.researchgate.net/profile/Zhen-Cheng/publication/311616883/figure/fig6/AS:482331262754821@1492008142177/a-Time-series-of-free-stream-velocity-in-which-four-representative-instants-are_Q320.jpg)
Velocity profiles at different locations downstream of the apron at (a)