Two wind tunnel tests during 1995 in the National Transonic Facility (NTF 070 and 073) served to define Reynolds number effects on longitudinal and lateral-directional stability and control. Testing was completed at both high lift and transonic conditions. The effect of Reynolds number on the total airplane configuration, horizontal and vertical tail effectiveness, forebody chine performance, rudder control and model aeroelastics was investigated. This paper will present pertinent stability and control results from these two test entries. Note that while model aeroelastic effects are examined in this presentation, no corrections for these effects have been made to the data.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    High Reynolds Number Effects on HSCT Stability and Control Characteristics




    Publication date :

    1999-12-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English