26th Congress of International Council of the Aeronautical Sciences
including the 8th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference
14 - 19 September 2008, Anchorage, Alaska, USA
Paper ICAS 2008-2.5.1

A CFD STUDY OF UCAV 1303 BASELINE MODEL AT CRUISE MACH NUMBERS

M. Khalid, W. Yuan, F. Zhang
NRC, Canada

Keywords: Unmanned Combat Air Vehicle, Blended Wing Body, CFD

This paper furnishes further computed results for the UCAV 1303 baseline model using the NPARC and FLOWer codes, at M = 0.35 and 0.85, AoA = 2.095-17.97 deg., Re = 4.1M and 7.2M, respectively. The computed results were agreeable to meassured data at lower angles of attack.

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