TY - GEN
T1 - Investigation of supersonic wing shape using busemann biplane airfoil
AU - Yonezawa, M.
AU - Yamashita, H.
AU - Obayashi, S.
AU - Kusunose, K.
PY - 2007
Y1 - 2007
N2 - Busemann biplane significantly reduces wave drag due to its thickness (or volume) at supersonic speeds using the shock wave interaction between the two wings. This paper investigates the influence of the three-dimensional effect to the rectangular wing using the biplane concept and considers the effects of various wing configurations which are a rectangular wing using a winglet, two tapered wing configurations and a Caret wing configuration based the Waverider concept.
AB - Busemann biplane significantly reduces wave drag due to its thickness (or volume) at supersonic speeds using the shock wave interaction between the two wings. This paper investigates the influence of the three-dimensional effect to the rectangular wing using the biplane concept and considers the effects of various wing configurations which are a rectangular wing using a winglet, two tapered wing configurations and a Caret wing configuration based the Waverider concept.
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M3 - Conference contribution
AN - SCOPUS:34250839413
SN - 1563478900
SN - 9781563478901
T3 - Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting
SP - 8482
EP - 8492
BT - Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting
T2 - 45th AIAA Aerospace Sciences Meeting 2007
Y2 - 8 January 2007 through 11 January 2007
ER -