Cummings, John C. (1974) Development of a high-performance cryogenic shock tube. Journal of Fluid Mechanics, 66 (1). pp. 177-187. ISSN 0022-1120. doi:10.1017/S0022112074000139. https://resolver.caltech.edu/CaltechAUTHORS:20120809-080934957
![[img]](https://authors.library.caltech.edu/style/images/fileicons/application_pdf.png)
|
PDF
- Published Version
See Usage Policy. 481kB |
Use this Persistent URL to link to this item: https://resolver.caltech.edu/CaltechAUTHORS:20120809-080934957
Abstract
A cryogenic shock tube has been developed as a tool for research in fluid mechanics and low-temperature physics. The shock tube was designed to operate with the test section immersed in a cryogenic liquid. A unique diaphragm-changing mechanism makes this shock tube an economical and practical device. There are several advantages in operating a shock tube at cryogenic temperatures. Shock waves of very large Mach number can be produced. The flow field can be accurately calculated using ideal-shock-tube/perfect-gas theory. Boundary-layer effects are decreased, so that long test times are possible.
| Item Type: | Article | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| Related URLs: |
| |||||||||
| Additional Information: | © 1974 Cambridge University Press. Received 19 February 1974. Published Online March 29 2006. This work was made possible by the U.S. Air Force Office of Scientific Research (Grant AFOSR 71-2092), and is based on part 1 of a thesis submitted in partial fulfillment of the requirements for a Ph.D. degree at the California Institute of Technology. The author wishes to acknowledge the many contributions to this work that were made by Prof. Hans W. Liepmann. | |||||||||
| Funders: |
| |||||||||
| Issue or Number: | 1 | |||||||||
| DOI: | 10.1017/S0022112074000139 | |||||||||
| Record Number: | CaltechAUTHORS:20120809-080934957 | |||||||||
| Persistent URL: | https://resolver.caltech.edu/CaltechAUTHORS:20120809-080934957 | |||||||||
| Official Citation: | John C. Cummings (1974). Development of a high-performance cryogenic shock tube. Journal of Fluid Mechanics, 66 , pp 177-187 doi:10.1017/S0022112074000139 | |||||||||
| Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. | |||||||||
| ID Code: | 33037 | |||||||||
| Collection: | CaltechAUTHORS | |||||||||
| Deposited By: | Ruth Sustaita | |||||||||
| Deposited On: | 09 Aug 2012 15:24 | |||||||||
| Last Modified: | 09 Nov 2021 21:31 |
Repository Staff Only: item control page
