Efficient fluid dynamic and structural design and integration method to achieve extended hybrid laminar flow control

Efficient fluid dynamic and structural design and integration method to achieve extended hybrid laminar flow control

Systems and methods for secondary suctioning for an aerodynamic body are presented. A primary surface is configured along a leading edge of an aerodynamic body, and at least one secondary suction device comprising an elongated shape is configured at least a first distance from the primary surface. A...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: LIAN L. NG, PRADIP G. PARIKH, PAUL M. VIJGEN, PETER L. RUPP
Format: Patent
Sprache:chi ; eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:Systems and methods for secondary suctioning for an aerodynamic body are presented. A primary surface is configured along a leading edge of an aerodynamic body, and at least one secondary suction device comprising an elongated shape is configured at least a first distance from the primary surface. A non-suction surface is configured between the primary surface and the at least one secondary suction device.