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Thrust coefficient

Thrust coefficient or c F {\displaystyle c_{F}} (sometimes c τ {\displaystyle c_{\tau }} ) is a dimensionless number that measures the performance of a nozzle, most commonly in a rocket engine, independent of combustion performance. It is often used to compare the performance of different nozzle geometries. After combining it with characteristic velocity…

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Thrust coefficient

Nodes22
Edges21
Triples8
Avg. degree1.91
Density0.090909
Components1

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Thrust coefficient

Top relations

related to Physics and context · 6
Thrust coefficient → Gadicharla, Rao, The, Thrust, Typical, Virtually
related to Corrections · 2
Thrust coefficient → Three, Various

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Important terminology

displaystyle nozzle thrust exhaust exit plane gas pressure frac coefficient velocity ideal left right gamma efficiency rocket engine combustion characteristic

Entity relationships Subject–Predicate–Object triples

SubjectPredicateObjectConfidenceSrc
Thrust coefficientrelated to CorrectionsVarious0.60section
Thrust coefficientrelated to CorrectionsThree0.60section
Thrust coefficientrelated to Physics and contextThrust0.60section
Thrust coefficientrelated to Physics and contextThe0.60section
Thrust coefficientrelated to Physics and contextTypical0.60section
Thrust coefficientrelated to Physics and contextVirtually0.60section
Thrust coefficientrelated to Physics and contextGadicharla0.60section
Thrust coefficientrelated to Physics and contextRao0.60section

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    Min side: 3
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