Mach number

E90366

Mach number is a dimensionless quantity in fluid dynamics and aerodynamics that expresses the ratio of an object's speed to the local speed of sound, commonly used to characterize subsonic, transonic, supersonic, and hypersonic flows.

AI illustration

How this image was made

AI-generated illustration of Mach number

This AI-generated illustration was produced by black-forest-labs/FLUX.2-dev (1024x1024) from a prompt written by openai/gpt-oss-120b from the entity's label + description.

Prompt

Generate an image of a mach number (Mach number is a dimensionless quantity in fluid dynamics and aerodynamics that expresses the ratio of an object's speed to the local speed of sound, commonly used to characterize subsonic, transonic, supersonic, and hypersonic flows.)

All labels observed (2)

Label Occurrences
Mach number canonical 4
Mach 2.5 1

How this entity was disambiguated

Statements (49)

Predicate Object
instanceOf aerodynamic parameter ⓘ
dimensionless quantity ⓘ
fluid dynamics parameter ⓘ
physical quantity ⓘ
alsoDenotedAs Ma ⓘ
definedAs ratio of flow speed to local speed of sound ⓘ
dependsOn flow velocity ⓘ
local speed of sound ⓘ
temperature of the medium ⓘ
thermodynamic properties of the fluid ⓘ
dimension dimensionless ⓘ
equalsOneMeaning sonic condition ⓘ
field aerodynamics ⓘ
fluid dynamics ⓘ
governs compressibility effects ⓘ
greaterThanOneMeaning supersonic condition ⓘ
influences aeroacoustic phenomena ⓘ
drag characteristics ⓘ
lift characteristics ⓘ
pressure distribution around bodies ⓘ
shock formation ⓘ
lessThanOneMeaning subsonic condition ⓘ
namedAfter Ernst Mach ⓘ
relatedConcept Froude number ⓘ
Knudsen number ⓘ
Reynolds number ⓘ
relatedTo speed of sound ⓘ
symbol M ⓘ
typicalRangeHypersonic M ≥ 5 ⓘ
typicalRangeSubsonic M < 0.8 ⓘ
typicalRangeSupersonic 1.2 < M < 5 ⓘ
typicalRangeTransonic 0.8 ≤ M ≤ 1.2 ⓘ
usedFor analyzing expansion waves ⓘ
analyzing shock waves ⓘ
classifying aircraft speed regimes ⓘ
classifying missile speed regimes ⓘ
classifying spacecraft atmospheric flight regimes ⓘ
nozzle flow characterization ⓘ
turbomachinery analysis ⓘ
wind tunnel testing conditions ⓘ
usedIn aerodynamic design ⓘ
compressible flow analysis ⓘ
gas dynamics ⓘ
high-speed aerodynamics ⓘ
usedToCharacterize aerodynamic regimes ⓘ
hypersonic flow ⓘ
subsonic flow ⓘ
supersonic flow ⓘ
transonic flow ⓘ

How these facts were elicited

Referenced by (5)

Full triples — surface form annotated when it differs from this entity's canonical label.

Ernst Mach → hasEponym → Mach number ⓘ
Mach cone → isRelatedTo → Mach number ⓘ
Mach → notableVersion → Mach 2.5 ⓘ
linked to: Mach number
Froude number → relatedTo → Mach number ⓘ