![How does the drag coefficient behave at transonic and supersonic speeds for swept wing aircraft? - Aviation Stack Exchange How does the drag coefficient behave at transonic and supersonic speeds for swept wing aircraft? - Aviation Stack Exchange](https://i.stack.imgur.com/6ZNaj.png)
How does the drag coefficient behave at transonic and supersonic speeds for swept wing aircraft? - Aviation Stack Exchange
![Elon Musk on Twitter: "@keithbigelow Very sensible summary of supersonic flight. Obvious answer is to fly high, which gives low drag & low boom amplitude at ground. If boom too loud, airframe Elon Musk on Twitter: "@keithbigelow Very sensible summary of supersonic flight. Obvious answer is to fly high, which gives low drag & low boom amplitude at ground. If boom too loud, airframe](https://pbs.twimg.com/media/DXapiw6V4AARcCv.jpg)
Elon Musk on Twitter: "@keithbigelow Very sensible summary of supersonic flight. Obvious answer is to fly high, which gives low drag & low boom amplitude at ground. If boom too loud, airframe
![Supersonic drag reduction technology in the scaled supersonic experimental airplane project by JAXA - ScienceDirect Supersonic drag reduction technology in the scaled supersonic experimental airplane project by JAXA - ScienceDirect](https://ars.els-cdn.com/content/image/1-s2.0-S0376042109000177-gr6.jpg)
Supersonic drag reduction technology in the scaled supersonic experimental airplane project by JAXA - ScienceDirect
![Institute of Aerodynamics and Flow Technology - Localized Flow Heating for Wave-Drag Reduction at Supersonic Speeds Institute of Aerodynamics and Flow Technology - Localized Flow Heating for Wave-Drag Reduction at Supersonic Speeds](https://www.dlr.de/as/en/Portaldata/5/Resources/images/abteilungen/abt_hk/artikel/Lokale_Stroemungserhitzung_zur_Bugwiderstandreduzierung-Bild1.jpg)
Institute of Aerodynamics and Flow Technology - Localized Flow Heating for Wave-Drag Reduction at Supersonic Speeds
![Supersonic drag reduction technology in the scaled supersonic experimental airplane project by JAXA - ScienceDirect Supersonic drag reduction technology in the scaled supersonic experimental airplane project by JAXA - ScienceDirect](https://ars.els-cdn.com/content/image/1-s2.0-S0376042109000177-gr3.jpg)
Supersonic drag reduction technology in the scaled supersonic experimental airplane project by JAXA - ScienceDirect
![aerodynamics - Why does drag coefficient decrease with Mach number in the supersonic regime? - Aviation Stack Exchange aerodynamics - Why does drag coefficient decrease with Mach number in the supersonic regime? - Aviation Stack Exchange](https://i.stack.imgur.com/Yzlxh.png)
aerodynamics - Why does drag coefficient decrease with Mach number in the supersonic regime? - Aviation Stack Exchange
![Sonic boom maximum pressure and wave drag coefficient with different S l . | Download Scientific Diagram Sonic boom maximum pressure and wave drag coefficient with different S l . | Download Scientific Diagram](https://www.researchgate.net/publication/274166026/figure/fig18/AS:667886678966275@1536248001364/Sonic-boom-maximum-pressure-and-wave-drag-coefficient-with-different-S-l.png)
Sonic boom maximum pressure and wave drag coefficient with different S l . | Download Scientific Diagram
![drag - Acceleration of a supersonic aircraft after breaking the sound barrier - Aviation Stack Exchange drag - Acceleration of a supersonic aircraft after breaking the sound barrier - Aviation Stack Exchange](https://i.stack.imgur.com/fB9ot.jpg)