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    Experimental study of tail-span effects on a generic canard-controlled missile (1992)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: An experimental investigation was conducted on a cruciform canard controlled missile configuration to determine the effects of tail span/canard span ratio on controllability. The investigation was conducted over the Mach number range of 1.75 to 3.50. Reductions of tail span/canard span ratio produced lower static margins and higher trim angle of attack. The results show that canard controls can provide pitch- and yaw-control as well as roll-control by proper selection of the tail span/canard span ratio.
    Keywords: AIRCRAFT STABILITY AND CONTROL
    Type: AIAA PAPER 92-0079
    Format: text
    Location Call Number Expected Availability
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