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by mshook
1848 days ago
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Not at all, the magic was in the intake which slowed down the air so the turbojet engine could use it. And that's why it was so efficient when flying at VMAX. Wiki again:
Forces from the internal airflow on the intake structure are rearwards (drag) on the initial converging section, where the supersonic deceleration takes place, and forwards on the diverging duct where subsonic deceleration takes place up to the engine entry. The sum of the 2 forces at cruise gave the 63% thrust contribution from the intake part of the propulsion system. https://en.wikipedia.org/wiki/Rolls-Royce/Snecma_Olympus_593 |
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