Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
shock wave
|
| gptkbp:angle_depends_on |
gptkb:Mach_number
deflection angle |
| gptkbp:can_be_generated_by |
cone
wedge airfoil |
| gptkbp:canBe |
attached
detached |
| gptkbp:cause |
decrease in Mach number
increase in pressure increase in temperature sudden change in flow properties |
| gptkbp:describes |
oblique shock relations
|
| gptkbp:distinctFrom |
gptkb:normal_shock_wave
|
| gptkbp:forms_at |
an angle to the direction of flow
|
| gptkbp:governs |
conservation of energy
conservation of momentum conservation of mass |
| https://www.w3.org/2000/01/rdf-schema#label |
oblique shock wave
|
| gptkbp:occurredIn |
supersonic flow
|
| gptkbp:studiedBy |
aerodynamics
gas dynamics |
| gptkbp:type |
compressible flow phenomenon
|
| gptkbp:used_in |
gptkb:supersonic_inlets
supersonic wind tunnels nozzle design |
| gptkbp:bfsParent |
gptkb:Prandtl–Meyer_expansion_fan
|
| gptkbp:bfsLayer |
6
|