File:Supersonic shockless fuselage.PNG
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Summary
| Description |
English: To generate lift a supersonic airplane has to produce at least two shock waves: One over-pressure downwards wave, and one under-pressure upwards wave. Withcomb’s area rule states, we can reuse air displacement without generating additional shock waves. In this case the fuselage reuses some displacement of the wings. |
| Date | |
| Source | various sources -> my head -> vector graphics -> png |
| Author | Arne Christian Rosenfeldt |
Licensing
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I, the copyright holder of this work, release this work into the public domain. This applies worldwide. In some countries this may not be legally possible; if so: I grant anyone the right to use this work for any purpose, without any conditions, unless such conditions are required by law. |
File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 12:05, 4 September 2005 | | 182 × 247 (9 KB) | Arnero | To generate lift a supersonic airplane has to produce at least two shock waves: One over-pressure downwards wave, and one under-pressure upwards wave. Withcomb’s area rule states, we can reuse air displacement without generating additional shock waves. |
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