Parametric Inlet Model in 10x10 Wind Tunnel
5 HOLE PROBE CALLIBRATION FOR 10X10 FOOT SUPERSONIC WIND TUNNEL AND 8X6 FOOT SUPERSONIC WIND TUNNEL COMPARISON TEST
UNSTART PROGRAM - 10X10 FOOT SUPERSONIC WIND TUNNEL AS PART OF THE HIGH SPEED RESEARCH PROGRAM
ROCKET BASED COMBINED CYCLE - RBCC - RIG 3.1 MODEL INSTALLED IN 10X10 FOOT SUPERSONIC WIND TUNNEL TEST SECTION
DAN KOVACH WORKING ON THE ROCKET BASED COMBINED CYCLE RIG 3.1 MODEL IN THE 10X10 FOOT SUPERSONIC WIND TUNNEL
NASA Glenn/NASA Langley, Loads Comparison Test With 6 Component Force/Moment Balance and 1.7% High Speed Research, HSR Model 5. In the Glenn Research Center 10x10 Foot Supersonic Wind Tunnel, SWT