Searching for aerodynamic data of the Space Shuttle

Hi everybody !

I'm an aerospace student at the Technische Universitaet Berlin, Germany. 
For my diploma thesis, I need some data about the aerodynamic of the Space 
Shuttle.
In detail, I need some information about the lift coefficient (cL) and the 
drag coefficient (cD) when the angle of attack (AoA) and mach number are 
given.

I searched for these data at the NASA site, the database of the Dryden 
Flight Research Center, the AICC, some libraries, but I didn't succeed.

Can anybody give my a hint, where I can find these data ?

Thanks a lot
Reiner

[Moderator: A good place to start is "Aerodynamic Design of the Space 
Shuttle Orbiter," in AGARD CP-247]