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- Bow_shock_(aerodynamics) abstract "A bow shock, also called a detached shock or normal shock, is a curved, stationary shock wave that is found in a supersonic flow past a finite body. The name comes from the example of a bow wave that forms at the bow of a ship when it moves through the water.Unlike an oblique shock, the bow shock is not necessarily attached to the tip of the body. Oblique shock angles are limited in formation and are based on the flow deflection angle, upstream Mach number. When these limitations are exceeded (greater deflection angle or lower Mach number), a detached bow shock forms instead of an oblique shock. As bow shocks form for high flow deflection angles, they are often seen forming around blunt objects.In other words, when the needed rotation of the fluid exceeds the maximum achievable rotation angle for an oblique attached shock, the shock detaches from the body. Downstream of the shock, the flow-field is subsonic, and the boundary condition can be respected at the stagnation point.The bow shock significantly increases the drag in a vehicle traveling at a supersonic speed. This property was utilized in the design of the return capsules during space missions such as the Apollo program, which need a high amount of drag in order to slow down during atmospheric reentry.".
- Bow_shock_(aerodynamics) thumbnail Bowshock_example_-_blunt_body.jpg?width=300.
- Bow_shock_(aerodynamics) wikiPageID "9212193".
- Bow_shock_(aerodynamics) wikiPageLength "2218".
- Bow_shock_(aerodynamics) wikiPageOutDegree "19".
- Bow_shock_(aerodynamics) wikiPageRevisionID "672431279".
- Bow_shock_(aerodynamics) wikiPageWikiLink Apollo_program.
- Bow_shock_(aerodynamics) wikiPageWikiLink Atmospheric_entry.
- Bow_shock_(aerodynamics) wikiPageWikiLink Atmospheric_reentry.
- Bow_shock_(aerodynamics) wikiPageWikiLink Bow_shocks_in_astrophysics.
- Bow_shock_(aerodynamics) wikiPageWikiLink Bow_wave.
- Bow_shock_(aerodynamics) wikiPageWikiLink Category:Aerodynamics.
- Bow_shock_(aerodynamics) wikiPageWikiLink Category:Shock_waves.
- Bow_shock_(aerodynamics) wikiPageWikiLink Compressible_flow.
- Bow_shock_(aerodynamics) wikiPageWikiLink Drag_(physics).
- Bow_shock_(aerodynamics) wikiPageWikiLink Elsevier.
- Bow_shock_(aerodynamics) wikiPageWikiLink Gas_dynamics.
- Bow_shock_(aerodynamics) wikiPageWikiLink Mach_number.
- Bow_shock_(aerodynamics) wikiPageWikiLink Moving_shock.
- Bow_shock_(aerodynamics) wikiPageWikiLink Oblique_shock.
- Bow_shock_(aerodynamics) wikiPageWikiLink Prandtl-Meyer_expansion_fan.
- Bow_shock_(aerodynamics) wikiPageWikiLink Prandtl–Meyer_expansion_fan.
- Bow_shock_(aerodynamics) wikiPageWikiLink Shock_wave.
- Bow_shock_(aerodynamics) wikiPageWikiLink Speed_of_sound.
- Bow_shock_(aerodynamics) wikiPageWikiLink Stagnation_point.
- Bow_shock_(aerodynamics) wikiPageWikiLink Supersonic.
- Bow_shock_(aerodynamics) wikiPageWikiLink Supersonic_speed.
- Bow_shock_(aerodynamics) wikiPageWikiLink File:Bowshock_example_-_blunt_body.jpg.
- Bow_shock_(aerodynamics) wikiPageWikiLinkText "Bow shock (aerodynamics)".
- Bow_shock_(aerodynamics) wikiPageWikiLinkText "Bow shocks".
- Bow_shock_(aerodynamics) wikiPageWikiLinkText "Bow".
- Bow_shock_(aerodynamics) wikiPageWikiLinkText "bow shock".
- Bow_shock_(aerodynamics) wikiPageWikiLinkText "bow shocks".
- Bow_shock_(aerodynamics) wikiPageWikiLinkText "shock wave".
- Bow_shock_(aerodynamics) hasPhotoCollection Bow_shock_(aerodynamics).
- Bow_shock_(aerodynamics) wikiPageUsesTemplate Template:Cite_book.
- Bow_shock_(aerodynamics) wikiPageUsesTemplate Template:Expert-subject.
- Bow_shock_(aerodynamics) wikiPageUsesTemplate Template:Fluiddynamics-stub.
- Bow_shock_(aerodynamics) subject Category:Aerodynamics.
- Bow_shock_(aerodynamics) subject Category:Shock_waves.
- Bow_shock_(aerodynamics) hypernym Wave.
- Bow_shock_(aerodynamics) type Band.
- Bow_shock_(aerodynamics) comment "A bow shock, also called a detached shock or normal shock, is a curved, stationary shock wave that is found in a supersonic flow past a finite body. The name comes from the example of a bow wave that forms at the bow of a ship when it moves through the water.Unlike an oblique shock, the bow shock is not necessarily attached to the tip of the body. Oblique shock angles are limited in formation and are based on the flow deflection angle, upstream Mach number.".
- Bow_shock_(aerodynamics) label "Bow shock (aerodynamics)".
- Bow_shock_(aerodynamics) sameAs m.0280ghq.
- Bow_shock_(aerodynamics) sameAs Q4950685.
- Bow_shock_(aerodynamics) sameAs Q4950685.
- Bow_shock_(aerodynamics) wasDerivedFrom Bow_shock_(aerodynamics)?oldid=672431279.
- Bow_shock_(aerodynamics) depiction Bowshock_example_-_blunt_body.jpg.
- Bow_shock_(aerodynamics) isPrimaryTopicOf Bow_shock_(aerodynamics).