Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:mathematical_concept
|
| gptkbp:appliesTo |
ideal gas
isentropic flow |
| gptkbp:describes |
expansion fan
|
| gptkbp:field |
fluid dynamics
|
| gptkbp:firstPublished |
1908
|
| gptkbp:form |
ν(M) = sqrt((γ+1)/(γ-1)) * arctan(sqrt((γ-1)(M^2-1)/(γ+1))) - arctan(sqrt(M^2-1))
|
| gptkbp:hasUnit |
gptkb:university
radian |
| https://www.w3.org/2000/01/rdf-schema#label |
Prandtl–Meyer function
|
| gptkbp:namedAfter |
gptkb:Ludwig_Prandtl
gptkb:Theodor_Meyer |
| gptkbp:output |
flow turning angle
|
| gptkbp:parameter |
specific heat ratio
|
| gptkbp:relatedTo |
gptkb:Mach_angle
gptkb:oblique_shock shock wave isentropic expansion |
| gptkbp:usedIn |
gas dynamics
supersonic flow |
| gptkbp:variant |
gptkb:Mach_number
|
| gptkbp:bfsParent |
gptkb:Prandtl–Meyer_expansion_fan
|
| gptkbp:bfsLayer |
6
|