Converging-Diverging Verification (CDV) Nozzle.

NASA Glenn Research Center. (2021). Converging-Diverging Verification (CDV) Nozzle. NPARC Alliance Validation Archive.

Type

Web resource

Intellectual base

Web

Year

2021

Link

https://www.grc.nasa.gov/www/wind/valid/cdv/cdv.html

Cited by

1 citation across 1 artifact.

Domain-specific

• Isentropic Nozzle Flow
  • Three exit-to-total pressure ratios deliberately produce different regimes: $0.89$ for subsonic isentropic flow, $0.75$ for a supersonic solution containing a normal shock, and $0.16$ for supersonic isentropic flow.

Verification

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Registry ID ref:de39c502636b · see in the full table