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High Reynolds Number Hybrid Laminar Flow Control (HLFC) Flight Experiment: Leading Edge Design, Fabrication, and Installation - 3This 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.
Document ID
19990052671
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Date Acquired
September 6, 2013
Publication Date
April 1, 1999
Subject Category
Aerodynamics
Report/Patent Number
NASA/CR-1999-209325
NAS 1.26:209325
Report Number: NASA/CR-1999-209325
Report Number: NAS 1.26:209325
Funding Number(s)
CONTRACT_GRANT: NAS1-18574
PROJECT: RTOP 522-32-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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