enow.com Web Search

Search results

  1. Results from the WOW.Com Content Network
  2. Template:Supersonic shockwave cone.svg - Wikipedia

    en.wikipedia.org/wiki/Template:Supersonic...

    Main page; Contents; Current events; Random article; About Wikipedia; Contact us; Donate

  3. File:Subsonic and trans-sonic airfoils.svg - Wikipedia

    en.wikipedia.org/wiki/File:Subsonic_and_trans...

    English: Subsonic (1) and trans-sonic (2) airfoils at identical Mach number. A: Supersonic flow region . B: Shock wave . C: Area of stalled flow . On the trans-sonic (or supercritical) airfoil, the deceleration of the flow on the top surface, and the strength of the shockwave with which the flow returns to a subsonic regime, are reduced.

  4. Template:Shock types - Wikipedia

    en.wikipedia.org/wiki/Template:Shock_types

    Main page; Contents; Current events; Random article; About Wikipedia; Contact us; Pages for logged out editors learn more

  5. File:Swept wing w supersonic shock.svg - Wikipedia

    en.wikipedia.org/wiki/File:Swept_wing_w...

    Main page; Contents; Current events; Random article; About Wikipedia; Contact us; Donate

  6. Inlet cone - Wikipedia

    en.wikipedia.org/wiki/Inlet_cone

    An inlet cone, as part of an Oswatitsch-type inlet used on a supersonic aircraft or missile, is the 3D-surface on which supersonic ram compression for a gas turbine engine or ramjet combustor takes place through oblique shock waves. Slowing the air to low supersonic speeds using a cone minimizes loss in total pressure (increases pressure recovery).

  7. Mach wave - Wikipedia

    en.wikipedia.org/wiki/Mach_wave

    Such a shock wave is called a Mach stem or Mach front. Thus, it is possible to have shockless compression or expansion in a supersonic flow by having the production of Mach waves sufficiently spaced (cf. isentropic compression in supersonic flows). A Mach wave is the weak limit of an oblique shock wave where time averages of flow quantities don ...

  8. Oblique shock - Wikipedia

    en.wikipedia.org/wiki/Oblique_shock

    An oblique shock at the nose of a T-38 aircraft is made visible through Schlieren photography. An oblique shock wave is a shock wave that, unlike a normal shock, is inclined with respect to the direction of incoming air. It occurs when a supersonic flow encounters a corner that effectively turns the flow into itself and compresses. [1]

  9. Taylor–Maccoll flow - Wikipedia

    en.wikipedia.org/wiki/Taylor–Maccoll_flow

    A conical shock wave can form in this situation, with the vertex of the shock wave lying at the vertex of the solid cone. If it were a two-dimensional problem, i.e., for a supersonic flow past a wedge, then the incoming stream would have deflected through an angle χ {\displaystyle \chi } upon crossing the shock wave so that streamlines behind ...