Apparatus and techniques were developed for measuring in a low-speed wind tunnel the static and dynamic (rotary balance) aerodynamic data pertinent to spin behavior of a general aviation aircraft. The main results were: (1) collection of static force and moment data for several airplane configurations at angles of attack from 0 to 90 degrees and angles of sideslip from 0 to 40 degrees; and (2) difficulties, shortcomings, and unsuitability of some aspects of the rotary balance mount as constructed were discovered and identified for avoidance in a new design for a mount.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Development of capabilities for stall/spin research


    Contributors:
    Craig, A. (author)

    Publication date :

    1976-06-20


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Stall/Spin Research Status Report

    Bowman, James S. / Burk, Sanger M. | SAE Technical Papers | 1974


    Stall/spin research status report

    Bowman, J. S., Jr. / Burk, S. M., Jr. | NTRS | 1974


    Development of High-Lift Mild-Stall UAV Airfoil with Post-Stall Flight Capabilities

    Abramov, D. / Klein, Y. / Shepshelovich, M. et al. | British Library Conference Proceedings | 2014


    Stall/spin awareness

    Stowell, Rich | TIBKAT | 2007