Flow Field and Stability of the Far Wake Behind Cylinders at Hypersonic Speeds

Flow Field and Stability of the Far Wake Behind Cylinders at Hypersonic Speeds

<p>An experimental study of the mean wake flow field and its stability has been carried out in the far wake of circular cylinders at a Mach number of 6. The Reynolds numbers ranged from 200 to 4000 with a few measurements at higher Reynolds number. Pitot pressure, static pressure and mean flow...

Full description

Bibliographic Details
Main Author: Behrens, Hermann Wilhelm
Format: Others
Published: 1966
Online Access:https://thesis.library.caltech.edu/5992/1/Behrens_hw_1966.pdf
Behrens, Hermann Wilhelm (1966) Flow Field and Stability of the Far Wake Behind Cylinders at Hypersonic Speeds. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/K0KH-9W58. https://resolver.caltech.edu/CaltechTHESIS:08172010-151639253 <https://resolver.caltech.edu/CaltechTHESIS:08172010-151639253>

Internet

https://thesis.library.caltech.edu/5992/1/Behrens_hw_1966.pdf
Behrens, Hermann Wilhelm (1966) Flow Field and Stability of the Far Wake Behind Cylinders at Hypersonic Speeds. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/K0KH-9W58. https://resolver.caltech.edu/CaltechTHESIS:08172010-151639253 <https://resolver.caltech.edu/CaltechTHESIS:08172010-151639253>

Similar Items