The F-16XL-2 Supersonic Laminar Flow Control Flight Test Experiment was part of the NASA High-Speed Research Program. The goal of the experiment was to demonstrate extensive laminar flow, to validate computational fluid dynamics (CFD) codes and design methodology, and to establish laminar flow control design criteria. Topics include the flight test hardware and design, airplane modification, the pressure and suction distributions achieved, the laminar flow achieved, and the data analysis and code correlation.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    F-16XL-2 Supersonic Laminar Flow Control Flight Test Experiment


    Beteiligte:
    S. G. Anders (Autor:in) / M. C. Fischer (Autor:in)

    Erscheinungsdatum :

    1999


    Format / Umfang :

    262 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    F-16XL-2 Supersonic Laminar Flow Control Flight Test Experiment

    Anders, Scott G. / Fischer, Michael C. | NTRS | 1999


    F-16XL Supersonic Laminar Flow Control Glove Flight Test Results

    Anderson, B. / Rowan, B. / AIAA | British Library Conference Proceedings | 1991