Tag: transonic flow

  • Shocks on a Wing

    Shocks on a Wing

    Commercial airliners fly in what is known as the transonic regime at Mach numbers between 0.8 and 1.0. While the airplane itself never exceeds the speed of sound, that doesn’t mean that there aren’t localized regions where air flows over the airplane at speeds above Mach 1. In fact, it’s actually possible sometimes to see shock waves on the top of airliner’s wings with nothing more than your eyes. The animations above show shock waves sitting about 50-60% of the way down the wing’s chord on a Boeing 737 (top) and Airbus A-320 (bottom). The shock wave looks like an unsteady visual aberration sitting a little ways forward of the wing’s control surfaces.

    The wings themselves are shaped so that these little shock waves are relatively stationary and remain upstream of the flaps pilots use for control. Otherwise, the sharp pressure change across a shock wave sitting over a control surface could make moving that surface difficult. This was one of the challenges pilots first trying to break the sound barrier faced. (Image credits: R. Corman, source; agermannamedhans, source)

  • Transonic Flow

    Transonic Flow

    In the transonic speed regime the overall speed of an airplane is less than Mach 1 but some parts of the flow around the aircraft break the speed of sound. The photo above shows a schlieren photograph of flow over an airfoil at transonic speeds. The nearly vertical lines are shock waves on the upper and lower surfaces of the airfoil. Although the freestream speed in the tunnel is less than Mach 1 upstream of the airfoil, air accelerates over the curved surface of airfoil and locally exceeds the speed of sound. When that supersonic flow cannot be sustained, a shock wave occurs; flow to the right of the shock wave is once again subsonic. It’s also worth noting the bright white turbulent flow along the upper surface of the airfoil after the shock. This is the boundary layer, which can often separate from the wing in transonic flows, causing a marked increase in drag and decrease in lift. Most commercial airliners operate at transonic Mach numbers and their geometry is specifically designed to mitigate some of the challenges of this speed regime.  (Image credit: NASA; via D. Baals and W. Corliss)

  • STS-135: The Final Shuttle Flight

    STS-135: The Final Shuttle Flight

    Condensation clouds form around sections of Atlantis as STS-135–the final space shuttle flight–launches from Cape Canaveral this morning. These clouds, also called Prandtl-Glauert singularities or vapor cones, form at transonic speeds when air accelerates around the vehicle. The area just behind these shock waves experiences a drop in pressure and temperature that brings a localized portion of the flow below the dew point. Rapid condensation of the moisture in the air results. Miss the launch? Watch it here.