AIRCRAFT, PROPULSION SYSTEM, AND INLET WITH SUPERSONIC COMPRESSION

AIRCRAFT, PROPULSION SYSTEM, AND INLET WITH SUPERSONIC COMPRESSION

Embodiments of an inlet, aircraft, and propulsion system includes an inlet spike with a compression surface configured to decelerate air flow from supersonic speed to subsonic speed before the air flow enters a cowling throat and diffuser section of the propulsion system.

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Bibliographische Detailangaben
Hauptverfasser: DAVIS ZACHARY S, HAJIC KENNETH J, ANDERSON JON T, KLINGE JOHN D
Format: Patent
Sprache:eng
Schlagworte:
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Beschreibung
Zusammenfassung:Embodiments of an inlet, aircraft, and propulsion system includes an inlet spike with a compression surface configured to decelerate air flow from supersonic speed to subsonic speed before the air flow enters a cowling throat and diffuser section of the propulsion system.