Construct · 1 fields · 1 citations

Rao optimum thrust contour: a standalone construct

One name. One construct. A landmark on the map.

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Rao optimumthrust contour1 CONSTRUCTRao optimum thrustRAO · AEROSPACE PROPULSION

A single standalone construct; nearby constructs are located against it in the Collider. Tap a field for its definition, unit, and measures.

Aerospace propulsion

a method for designing a bell nozzle wall contour that maximizes thrust for a given length and area ratio.

In aerospace propulsion, Rao optimum thrust contour refers to a method for designing a bell nozzle wall contour that maximizes thrust for a given length and area ratio. This meaning comes from Rao (1958) in Journal of Jet Propulsion.[1]

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Nearby constructs

contour2 fields · 4 citationsjingle · one word, two constructsthrust2 fields · 2 citationsjingle · one word, two constructs

References

  1. Rao, G. V. R. (1958). Exhaust Nozzle Contour for Optimum Thrust. Journal of Jet Propulsion, 28(6), 377-382. https://doi.org/10.2514/8.7324

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