AGARD-B standard model is intended primarily for the measurement of aerodynamic forces and moments. Test results are most often presented in the form of nondimensional aerodynamic coefficients in the wind axes system. Reference area for the calculation of the coefficients is the theoretical wing area S ref = 4 √ 3 D. Reference length for the pitching moment coefficient C m is the mean aerodynamic chord (m.a.c.) equal to 4 √ 3 D/3 while the reference length for the yawing and rolling moment coefficients C n and C l is the wing span (B ref = 4 D). Moments are reduced to a point in the plane of symmetry of the model, at the longitudinal position of 50% of the m.a.c. (however, in some published results, moments were reduced to a point at 25% of the m.a.c.). Drag coefficient is presented in terms of forebody drag C xf obtained by subtracting, from the total measured drag C x, the base drag C xb computed from the measured base pressure on the model. Likewise, Lift coefficient represents forebody lift.