Aerodynamic loads on a sting mounted 0.045-scale representation of the 140C outer mold line space shuttle orbiter configuration were measured to verify orbiter landing gear system pressure loading and hinge moment levels. Pressure, force, and hinge moment data, recorded over smaller increments of the landing gear deployment schedule to insure data accuracy and to investigate the effects of asymmetric gear deployment on all parameters, are presented. Tests were conducted at a Mach number of 0.17, and freestream dynamic pressure of 42.5 psf, and a Reynolds number per unit length of 1.2 million foot. Angle of attack variation was -2 to 10 degrees while angles of sideslip varied from -5 to 5 degrees.


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    Titel :

    Results of a Landing Gear Loads Test Using a 0.0405-Scale Model (16-0) of the Space Shuttle Orbiter in the Rockwell International Naal Wind Tunnel (Oa163b), Volume 1


    Beteiligte:
    R. C. Mennell (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    756 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch