Abstr:Shock/boundary-layer interaction (on airplanes): Revision history

14 January 2022

• curprev 11:4711:47, 14 January 2022‎ Joe.Morris talk contribs‎ m 7,634 bytes −275‎ Removed semantic markup.

19 October 2011

• curprev 10:4210:42, 19 October 2011‎ Dave.Ellacott talk contribs‎ 7,909 bytes +48‎ No edit summary

29 August 2009

• curprev 12:3112:31, 29 August 2009‎ Niek.verhoeven talk contribs‎ 7,861 bytes +5‎ No edit summary
• curprev 11:3411:34, 29 August 2009‎ Niek.verhoeven talk contribs‎ 7,856 bytes +189‎ No edit summary

28 August 2009

• curprev 17:1217:12, 28 August 2009‎ Niek.verhoeven talk contribs‎ 7,667 bytes −4‎ No edit summary

7 April 2009

• curprev 13:0713:07, 7 April 2009‎ Daveg talk contribs‎ m 7,671 bytes 0‎ Shock/boundary-layer interaction (on airplanes) moved to Abstr:Shock/boundary-layer interaction (on airplanes)

6 March 2009

• curprev 11:4411:44, 6 March 2009‎ David.Fowler talk contribs‎ m 7,671 bytes +592‎ No edit summary

23 May 2008

• curprev 08:1608:16, 23 May 2008‎ Daveg talk contribs‎ 7,079 bytes +7,079‎ New page: ==Semi-Confined Flows== ===Underlying Flow Regime 3-05=== ====Abstract==== The interaction of a shock with a boundary layer developing on an aircraft wing can have an enormous impact on ...