A wind-tunnel investigation was made to determine the characteristics of spoiler ailerons used as speed brakes or glide-path controls on an NACA 65- 210 wing and an NACA 65-215 wing equipped with full-span slotted flaps. Several plug-aileron and retractable-aileron configurations were investigated on the two wing models with the full-span flaps retracted and deflected. Tests were made at various Mach numbers between 0.13 and 0.71.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Investigation of Spoiler Ailerons for use as Speed Brakes or Glide-Path Controls on Two NACA 65-Series Wings Equipped with Full-Span Slotted Flaps


    Contributors:
    J. Fischel (author) / J. M. Watson (author)

    Publication date :

    1949


    Size :

    61 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English