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- Shock_stall abstract "A shock stall is a stall created when the airflow over an aircraft's wings is disturbed by shock waves formed when flying at or above the aircraft's drag divergence Mach number.A stall is the decrease in Lift to a value below the Weight, and the associated increase in Drag upon the separation of the boundary layer (in this case behind the shock wave).".
- Shock_stall wikiPageID "1639361".
- Shock_stall wikiPageLength "472".
- Shock_stall wikiPageOutDegree "7".
- Shock_stall wikiPageRevisionID "665212042".
- Shock_stall wikiPageWikiLink Aircraft.
- Shock_stall wikiPageWikiLink Airflow.
- Shock_stall wikiPageWikiLink Category:Aerodynamics.
- Shock_stall wikiPageWikiLink Drag_divergence_Mach_number.
- Shock_stall wikiPageWikiLink Shock_wave.
- Shock_stall wikiPageWikiLink Stall_(fluid_mechanics).
- Shock_stall wikiPageWikiLink Wing.
- Shock_stall wikiPageWikiLinkText "Shock stall".
- Shock_stall wikiPageWikiLinkText "shock stall".
- Shock_stall wikiPageUsesTemplate Template:Aviation-stub.
- Shock_stall subject Category:Aerodynamics.
- Shock_stall hypernym Stall.
- Shock_stall type Dynamic.
- Shock_stall comment "A shock stall is a stall created when the airflow over an aircraft's wings is disturbed by shock waves formed when flying at or above the aircraft's drag divergence Mach number.A stall is the decrease in Lift to a value below the Weight, and the associated increase in Drag upon the separation of the boundary layer (in this case behind the shock wave).".
- Shock_stall label "Shock stall".
- Shock_stall sameAs Q7499880.
- Shock_stall sameAs m.05jsk9.
- Shock_stall sameAs Q7499880.
- Shock_stall wasDerivedFrom Shock_stall?oldid=665212042.
- Shock_stall isPrimaryTopicOf Shock_stall.