FIGURE 12
Different parts of the A321NEO aircraft considered in the installed performance analysis to identify the sources of multipath: a) fuselage only; b) fuselage and tail; c) fuselage, tail, and wings (without winglets); and d) full aircraft
Different parts of the A321NEO aircraft considered in the installed performance analysis to identify the sources of multipath: a) fuselage only; b) fuselage and tail; c) fuselage, tail, and wings (without winglets); and d) full aircraft