<--- Back to Details
First PageDocument Content
Dynamics / Aerospace engineering / Ludwieg tube / Mach reflection / Mach number / Supersonic speed / Mach wave / Compressible flow / Gas dynamics / Fluid dynamics / Aerodynamics / Fluid mechanics
Date: 2012-12-25 21:26:56
Dynamics
Aerospace engineering
Ludwieg tube
Mach reflection
Mach number
Supersonic speed
Mach wave
Compressible flow
Gas dynamics
Fluid dynamics
Aerodynamics
Fluid mechanics

Add to Reading List

Source URL: thesis.library.caltech.edu

Download Document from Source Website

File Size: 4,72 MB

Share Document on Facebook

Similar Documents

J. Fluid Mech[removed]), vol. 750, pp. 385_400. c Cambridge University Press 2014 doi:[removed]jfm[removed]Dynamic transition from Mach to regular reflection of shock waves in a steady flow K. Naidoo1 and B. W. Skews2,†

J. Fluid Mech[removed]), vol. 750, pp. 385_400. c Cambridge University Press 2014 doi:[removed]jfm[removed]Dynamic transition from Mach to regular reflection of shock waves in a steady flow K. Naidoo1 and B. W. Skews2,†

DocID: Mi9O - View Document

THREE-DIMENSIONAL, SHOCK-ON-SHOCK INTERACTION PROBLEM* By Paul Kutler NASA Ames Research Center and  Leonidas Sakell

THREE-DIMENSIONAL, SHOCK-ON-SHOCK INTERACTION PROBLEM* By Paul Kutler NASA Ames Research Center and Leonidas Sakell

DocID: M2Uh - View Document

8th International Conference on Multiphase Flow ICMF 2013, Jeju, Korea, May 26–31, 2013 Droplet Breakup in High-Speed Gas Flows Jomela C. Meng1 and Tim Colonius2 1

8th International Conference on Multiphase Flow ICMF 2013, Jeju, Korea, May 26–31, 2013 Droplet Breakup in High-Speed Gas Flows Jomela C. Meng1 and Tim Colonius2 1

DocID: zm9d - View Document

QM13: The Observability of Counterfactuals The Elitzur-Vaidman Bomb Test, Ref.[1] Last Update: [removed]

QM13: The Observability of Counterfactuals The Elitzur-Vaidman Bomb Test, Ref.[1] Last Update: [removed]

DocID: 4J4u - View Document

PDF Document

DocID: 1yFU - View Document