A shock wave detection system includes a light beam emitter, a light beam receiver and an analysis unit. The light beam emitter emits a light beam oblique to a direction of an air flow through which a shock wave may propagate. The light beam receiver receives the light beam that has passed through the air flow. The analysis unit is configured to detect a presence and a position of the shock wave based on a change in a receiving position of the light beam by the light beam receiver.
SHOCK WAVE DETECTION SYSTEM, METHOD OF DETECTING SHOCK WAVE AND AIRCRAFT
28.03.2024
Patent
Elektronische Ressource
Englisch
Shock wave noise of supersonic aircraft
Engineering Index Backfile | 1960
|SHOCK WAVE NOISE OF SUPERSONIC AIRCRAFT
SAE Technical Papers | 1960
|