TY - GEN
T1 - Reduction of aerodynamic interference for separation of two-stage reusable launch vehicles
AU - Uematsu, Taro
AU - Ishida, Takuro
AU - Aso, Shigeru
AU - Tani, Yasuhiro
PY - 2009
Y1 - 2009
N2 - In this paper, we focused on reduction of reflected shock wave generated between two bodies in hypersonic flow field. Problem of the flow field was modeled as flow field between the flat plate with wedge-shaped at the top and slender body in hypersonic flow field. The slender body has three cross section configuration patterns (circle, triangle and square). We carried out 3-D numerical calculation for the modeled flow field and conducted wind tunnel experiment. From their results, the slender body having triangle cross section can reduce the reflected shock wave.
AB - In this paper, we focused on reduction of reflected shock wave generated between two bodies in hypersonic flow field. Problem of the flow field was modeled as flow field between the flat plate with wedge-shaped at the top and slender body in hypersonic flow field. The slender body has three cross section configuration patterns (circle, triangle and square). We carried out 3-D numerical calculation for the modeled flow field and conducted wind tunnel experiment. From their results, the slender body having triangle cross section can reduce the reflected shock wave.
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M3 - Conference contribution
AN - SCOPUS:78549282130
SN - 9781563479694
T3 - 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
BT - 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
T2 - 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
Y2 - 5 January 2009 through 8 January 2009
ER -