An experimental research program establishing a database of the surfac
e pressure in swept shock wave/boundary-layer interactions is describe
d. An equilibrium turbulent boundary-layer on a flat plate is subjecte
d to impingement by swept planar shock waves genterated by a sharp fin
. Various fin angles at 4 different freestream Mach numbers produce a
variety of interaction strengths from weak to very strong. For each of
different interaction cases, the surface flow patterns are obtained b
y a kerosene-lampblack-adhesive transparent tape technique. Surface pr
essures within the interactions are also measured from several streamw
ise row of taps connected to a computer-controlled Scanivalve system.
An extensive error analysis is carried out for the experiments yieldin
g an uncertainty of about +/- 3%. From these measurements, high spatia
l resolution surface pressure distributions for different interaction
cases are obtained.