Construct · 1 fields · 1 citations

Lenoir-Robillard model: a standalone construct

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

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Aerospace propulsion

a model of erosive burning that adds a convective heat transfer term from the core gas flow to the pressure-dependent solid propellant burning rate.

In aerospace propulsion, Lenoir-Robillard model refers to a model of erosive burning that adds a convective heat transfer term from the core gas flow to the pressure-dependent solid propellant burning rate. This meaning comes from Lenoir (1957) in Symposium (International) on Combustion.[1]

Unit
Recovery means
Measured by

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Nearby constructs

erosive burning1 fields · 1 citationsanchor · a standalone construct flow6 names · 12 citationsjangle · five names, one experience, partly heat2 fields · 2 citationsjingle · one word, two constructs

References

Lenoir, J. M., & Robillard, G. (1957). A mathematical method to predict the effects of erosive burning in solid-propellant rockets. Symposium (International) on Combustion, 6(1), 663-667. https://doi.org/10.1016/s0082-0784(57)80092-7

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