With the help of hundreds of pressure
transducers, engineers from Sierra Nevada Corporation, the United Launch
Alliance and NASA Langley will look at the pressure fluctuations the model and
launch vehicle stack experience during the critical ascent to orbit, especially
at transonic speeds. Shock-waves form on launch vehicles as they approach the
speed of sound and may result in regions of highly unsteady flow. Within these
regions of the Dream Chaser and launch vehicle, the resulting buffet forces and
high frequency acoustic noise must be clearly understood as part of the vehicle
design process. Transonic wind-tunnel testing of large, highly instrumented
scale models is the only method of determining the buffet environments of
launch vehicles with complex shapes.
Image Credit: NASA EDGE/Ron Beard
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