Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:shock_wave
|
| gptkbp:angle_depends_on |
deflection angle
upstream Mach number |
| gptkbp:canBe |
attached
detached |
| gptkbp:cause |
decrease in Mach number
increase in pressure increase in temperature |
| gptkbp:contrastsWith |
normal shock
|
| gptkbp:describedBy |
oblique shock relations
|
| gptkbp:field |
fluid dynamics
aerodynamics |
| gptkbp:governedBy |
conservation of energy
conservation of momentum conservation of mass |
| gptkbp:occurredIn |
supersonic flow encounters a compression corner
|
| gptkbp:used_in |
gptkb:supersonic_inlets
aerospace engineering nozzle design |
| gptkbp:bfsParent |
gptkb:Shock_Waves
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
oblique shock
|