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Supersonic drag reduction technology in the scaled supersonic experimental airplane project by JAXA - ScienceDirect
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Institute of Aerodynamics and Flow Technology - Localized Flow Heating for Wave-Drag Reduction at Supersonic Speeds
![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
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Sonic boom maximum pressure and wave drag coefficient with different S l . | Download Scientific Diagram
![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
![PDF] A New Supersonic Wing Far-Field Composite Element Wave Drag Optimization Method , “ FCE ” | Semantic Scholar PDF] A New Supersonic Wing Far-Field Composite Element Wave Drag Optimization Method , “ FCE ” | Semantic Scholar](https://d3i71xaburhd42.cloudfront.net/844d0f43090d142cb1fbf051cde0ae49f134ed90/7-Figure6-1.png)