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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    High Reynolds Number Hybrid Laminar Flow Control (HLFC) Flight Experiment, 3


    Publication date :

    1999


    Size :

    92 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English