GONG Jun-feng, ZHU Xiao-ping, TAO Yu-jin. Split drag rudder hinge moment predict for flying wing aircraft[J]. ACTA AERODYNAMICA SINICA, 2010, 28(4): 472-477.
Citation: GONG Jun-feng, ZHU Xiao-ping, TAO Yu-jin. Split drag rudder hinge moment predict for flying wing aircraft[J]. ACTA AERODYNAMICA SINICA, 2010, 28(4): 472-477.
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Split drag rudder hinge moment predict for flying wing aircraft

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