Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft_component
|
| gptkbp:designedFor |
minimize total pressure loss
prevent engine surge |
| gptkbp:enables |
efficient engine operation at supersonic speeds
|
| gptkbp:example |
Concorde inlet
SR-71 Blackbird inlet |
| gptkbp:feature |
shock waves
variable geometry bleed air systems movable ramps spikes or cones |
| gptkbp:function |
increase pressure of incoming air
slow down supersonic airflow |
| gptkbp:relatedTo |
turbojet engines
ramjet engines scramjet engines |
| gptkbp:type |
external compression inlet
internal compression inlet mixed compression inlet |
| gptkbp:usedIn |
supersonic aircraft
|
| gptkbp:bfsParent |
gptkb:oblique_shock
gptkb:oblique_shock_wave |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
supersonic inlets
|