Advances in Aerodynamics

Table 2 Comparison of force coefficients for DLR-F6 wing-body configuration

From: A three-dimensional gas-kinetic flux solver for simulation of viscous flows with explicit formulations of conservative variables and numerical flux

References	C_l	C_{d, p}	C_{d, f}	C_d	C_M
Vassberg et al. [46]	0.51600	0.01502	0.01229	0.02731	−0.15280
Yang et al. [48]	0.52312	0.01554	0.00979	0.02533	−0.14988
Present	0.52470	0.01549	0.00947	0.02496	−0.16230

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