Mach number
flowchart AA["Associated Authors (1)"] C[Mach number] BC["Broader Concepts (3)"] NC["Narrower Concepts (9)"] C== skos:broader ==>BC NC== skos:broader ==>C AA== dcterms:relation ==>C click BC "#broader-concepts" click NC "#narrower-concepts" click AA "#associated-authors" NI["add incoming edge"] NO["add outgoing edge"] NI-- ? -->C C-- ? -->NO click NI "#add-incoming-edge" click NO "#add-outgoing-edge" style NI stroke-width:2px,stroke-dasharray: 5 5 style NO stroke-width:2px,stroke-dasharray: 5 5
- Wikidata
- https://www.wikidata.org/wiki/Q160669
- OpenAlex ID
- https://openalex.org/C165231844 (API record)
- OpenAlex Description
- ratio of speed of object moving through fluid and speed of sound
- OpenAlex Level [?]
- 2
Broader Concepts
Narrower Concepts
- Expansion tunnel
- Hypersonic flight
- Hypersonic flow
- Hypersonic wind tunnel
- Mach wave
- Oblique shock
- Stagnation enthalpy
- Stagnation pressure
- Supersonic wind tunnel
Associated Authors
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