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    Wind-Tunnel Investigation of a Full-Scale Model of the Hughes MX-904 Missile (1950)
    In:  CASI
    Details
    Publication Date: 2019-07-11
    Description: A wind-tunnel investigation has been conducted to determine the stability and control characteristics of a full-size model of the Hughes MX-904 missile. Aerodynamic characteristics of the complete model through moderate ranges of angles of attack and yaw, with an additional test made through an angle of attack of 180 degrees, are presented. The effects of horizontal tail deflection are also included.
    Keywords: Aircraft Design, Testing and Performance
    Type: NACA-RM-SL9D28
    Format: application/pdf
    Location Call Number Expected Availability
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