This document describes the design, fabrication, and installation of the suction panel and the required support structure, ducting, valving, and high-lift system (Krueger flaps) for flight demonstration of hybrid laminar flow control on the Boeing 757 airplane.
High Reynolds Number Hybrid Laminar Flow Control (HLFC) Flight Experiment, 3
1999
92 pages
Report
No indication
English
Flight Operational Assessment of Hybrid Laminar Flow Control (HLFC) Aircraft
British Library Conference Proceedings | 2001
|Investigation of hybrid laminar flow control (HLFC) surfaces
Online Contents | 2001
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