Normal Shock Verification.

NASA Glenn Research Center. (2021). Normal Shock Verification. NPARC Alliance Validation Archive.

Type

Web resource

Intellectual base

Web

Year

2021

Link

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

Cited by

1 citation across 1 artifact.

Domain-specific

• Isentropic Nozzle Flow
  • A normal shock can stand downstream of a sonic throat; the flow is adiabatic across the shock but irreversible, entropy rises, and stagnation pressure falls.

Verification

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Registry ID ref:2ee785705736 · see in the full table