Yes and the US has ample test data from the 60's, 70's and the 80's that they had collected during the various X-projects and others requiring hyper speed projectiles and flying objects.
The US designed the SR-71 supersonic planes in the 60's and flown the X-15 at speeds of Mach 6.7 in the late 60's as well.
Those data are now used to calculate simulations.
Like I posted within my original post, computer SIMULATION is used for the DESIGNING PHASE to weed out bad designs. This is the same with any other CFD projects in any industry.
Once they have reached the final stage (prototype) it is more constructive to just strap it on to a rocket and fly it at hyper sonic stage then testing it in a wind tunnel that can only give you a mili-second worth of data since that is about the only amount you can get from a hyper sonic wind tunnel. (They basically blast an explosive charge and direct the blast force towards the test piece to obtain the testing speeds so it cannot sustain speeds for more than a few mili-seconds)
In that case explain me this.