MITIGATION OF ADVERSE FLOW CONDITIONS IN A NACELLE INLET

The invention relates to mitigation of adverse flow conditions in a nacelle inlet. An airflow proximate to leading edges of a turbofan nacelle is ejected substantially normal to a fan face of the turbofan, creating suction proximate to the leading edge and mitigating flow separation proximate to the...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	PALACIOS GUTIERREZ FRANCISCO DE ASIS, HOISINGTON ZACHARY CHARLES, BROWN ERIC DAVID
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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