Wind tunnels can simulate scramjet speeds, specifically between Mach 6-12, but the test durations are typically very short due to the high pressures required. Facilities like NASA Glenn Research Center can reach Mach 5-7 for about five minutes. Testing high-velocity air-breathing engines is conducted in these wind tunnels, as untested engines would not be safely flown on aircraft. However, achieving accurate simulation requires matching Mach number, Reynolds number, and stagnation enthalpy, which is challenging and often results in compromises. Overall, while wind tunnels can simulate scramjet conditions, achieving precise testing parameters remains complex.