1. High-Reynolds-Number Cryogenic Wind Tunnel
2. 3) Cook, W. J. and Woicke, D. E.: Shock Tube Study of NACA 0012 Airfoil Flows for Air and SF6 in A Test Section with Straight Walls, ISU ERI Report, No. 95402, July 15 (1994).
3. 4) Yamaguchi, Y.: Performance of a Slotted Wall Test Section for Aerodynamic Testing in a Shock Tube, Theor. Appl. Mech., 37 (1989), pp. 39–47.
4. Airfoil Flow Visualization and Pressure Measurements in High-Reynolds-Number Transonic Flow