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nozzle thrust coefficient |
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nozzle thrust coefficient [′näz·əl ¦thrəst ‚kō·i‚fish·ənt]
(aerospace engineering) A measure of the amplification of thrust due to gas expansion in a particular nozzle as compared with the thrust that would be exerted if the chamber pressure acted only over the throat area. Also known as thrust coefficient. Want to thank TFD for its existence? Tell a friend about us, add a link to this page, add the site to iGoogle, or visit the webmaster's page for free fun content. |
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