Preliminary results are presented of a study conducted to analyze the effects of several planform modifications on the aerodynamic characteristics of a high-aspect-ratio, natural laminar flow (NLF) wing. The study addresses the potential aerodynamic improvements available at both cruise and high angles of attack by use of swept wing-tip shapes. The swept wing tip appears to offer a viable addition to the lift of wing-tip designs which provide improvements in aerodynamic efficiency, with the added safety benefit of providing high angle-of-attack departure resistance.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Swept Wing-Tip Shapes for Low-Speed Airplanes


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    van Dam, C. P. (Autor:in)

    Kongress:

    Aerospace Technology Conference and Exposition ; 1985



    Erscheinungsdatum :

    01.10.1985




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Prediction of downwash behind swept-wing airplanes at subsonic speed

    DeYoung, J. / Barling, Jr., W.H. | Engineering Index Backfile | 1955


    Prediction of Downwash Behind Swept-wing Airplanes at Subsonic Speed

    Deyoung, John / Barling, Warter H , Jr | NTRS | 1955


    Prediction of downwash behind swept-wing airplanes at subsonic speed

    DeYoung, John / Barling, Walter H. | TIBKAT | 1955


    Forward Swept Wings and Business Airplanes

    Roskam, Jan | SAE Technical Papers | 1980