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
Add Incoming Edge
Login via ORCiD to contribute.
Add Outgoing Edge
Login via ORCiD to contribute.
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