Construct · 1 fields · 1 citations

Lenoir-Robillard model: a standalone construct

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

● anchor · a standalone construct Nearest construct by meaning·not indexed
Lenoir-Robillardmodel1 CONSTRUCTLenoir-Robillard modelLENOIR · 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 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

Next

Run it through the Collider, or take the citations with you.

See how Lenoir-Robillard model sits against neighbouring constructs in the Collider, or export every reference on this page in one click.

Open in ColliderExport BibTeXReport this entry

Nearby constructs

erosive burning1 fields · 1 citationsanchor · a standalone constructflow6 names · 12 citationsjangle · five names, one experience, partlyheat2 fields · 2 citationsjingle · one word, two constructs

References

  1. 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

Cited on this page?

Confirm your construct, or correct us.

If your work is cited behind one of these entries, you know better than we do whether we captured the meaning right. Confirm it, suggest an edit, or dispute it, and your name goes on the entry as an author who has checked it, linked to your ORCID.

Claim your construct