This handbook is a sequel to an earlier volume entitled "A Theory of
Supercritical Wing Sections, with Computer Programs and Examples." Since
the completion of the first volume, which we shall refer to as Volume I
(cf. [ll), some effort has been made to improve our airfoil design
program. A number of more desirable air- foils have been designed. In
addition several of our wing sections have been tested in wind tunnels.
We should like to make this material available here, since it is more
convenient to use the design program in conjunction with data for a
fairly broad range of examples. Moreover, we have developed new analysis
programs that supersede our previous work. Chapter I is devoted to a
brief discussion of the mathematics involved in our additions and
modifications. There is only a mini- mum emphasis on theory, since the
representation of important physical phenomena such as boundary layer
shock wave interaction and separation is partly empirical. It is our
contention, however, that the computer programs provide a better
simulation than might have been expected. Chapter II presents numerical
results found by our new methods, as well as comparisons with
experimental data. Chapter III contains a discussion of the use of the
program together with Fortran listings.