OPTIMIZATION of wing design aims at finding the best compromise between conflicting aerodynamic requirements and considerations of structure weight and stiffness. Since the profile drag of a laminarizcd aircraft is very small, the induced drag has to be correspondingly reduced for proper matching. Reduction of induced drag can only be obtained, for a given dynamic pressure at the cruise, by increasing the span, and that reflects on structure weight.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Boundary Layer Control for Low Drag


    Untertitel :

    A Review of the Present Situation and an Assessment of the Potentialities of Laminarization Techniques


    Beteiligte:
    Lachmann, G.V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962-04-01


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Boundary-Layer Control for Drag Reduction

    Harvey, William D. | SAE Technical Papers | 1987


    Boundary layer control for low drag

    Lachmann, G.V. | Engineering Index Backfile | 1962


    Drag, Viscosity, and the Boundary Layer

    Smetana, Frederick O. | AIAA | 1997


    Drag Reduction by Use of MHD Boundary-Layer Control

    Gordon F. Anderson / Yung-Kuang Wu | AIAA | 1971


    Flight experiments on boundary layer control for low drag

    Head, Malcolm Robert ;Johnson, D. ;Coxon, M. | SLUB | 1957