27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-4.8.3

2D AND 3D INTAKES PERFORMANCE AND DRAG OF CRUISE M=1.6 CIVIL AIRCRAFT

V. A. Vinogradov, V. A. Stepanov
CIAM, Russian Federation

Keywords: 2d and 3d intake, drag, throttle performance

Designing and numerical study of flow field peculiarities and intake performance including internal ones and drag (additional and spillage) of traditional 2D scheme and 3D scheme for supersonic cruise M=1.6 civil aircraft are considered at Mach number flight region M=0.8-1.8.

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