Jump to content

Mach wave: Revision history


For any version listed below, click on its date to view it. For more help, see Help:Page history and Help:Edit summary. (cur) = difference from current version, (prev) = difference from preceding version, m = minor edit, → = section edit, ← = automatic edit summary

(newest | oldest) View (newer 50 | ) (20 | 50 | 100 | 250 | 500)

21 March 2024

22 March 2023

8 March 2023

12 February 2023

23 July 2022

17 March 2022

15 March 2022

20 June 2021

31 December 2020

9 May 2020

12 October 2018

27 November 2017

27 January 2017

  • curprev 20:1920:19, 27 January 2017 Astralnocturne talk contribs m 2,364 bytes +15 Corrected minor error with the velocity inferred from the photo. I measured the shock angle off the nose as about 59 degrees, using a protractor. So, mu = 59 deg. Using the mach angle formula, the mach number M = 1/sin(59 deg) = 1.1666, or about 1.17. undo

30 November 2016

26 April 2016

25 April 2016

4 March 2016

13 December 2015

9 October 2015

25 October 2014

16 September 2014

27 February 2014

28 March 2013

27 March 2013

26 March 2013

11 March 2013

8 March 2013

7 December 2012

28 June 2012

  • curprev 11:0211:02, 28 June 2012 2.229.28.88 talk 2,736 bytes −1 to get a condensation you need a DECREASE in pressure (which causes an adiabatic decrease in Temperature): actually, the Shock wave consists of an initial increase in pressure followed by a decrease (the so-called N-wave) undo

3 December 2011

5 November 2011

20 August 2010

12 May 2010

3 May 2010

20 January 2010

15 November 2009

30 September 2009

27 September 2009

19 August 2009

8 April 2009

11 February 2009

20 October 2008

20 March 2008

(newest | oldest) View (newer 50 | ) (20 | 50 | 100 | 250 | 500)