The aerodynamic data for two kinds of elliptic-cone derived waveriders
are presented and analyzed for a wide range of Mach numbers and angle
s of attack. The basic shapes of the waveriders are obtained by means
of hypersonic small-disturbance theory. Various off-design performance
s of the waveriders as well as on-design performances are obtained and
fully discussed. These aerodynamic data are informative for the desig
n of hypersonic airplanes which are being investigated as future plane
s. Also from the entropy distributions across the shock layers for ell
iptic-cones and waveriders, the vortical layer is analyzed and discuss
ed.