Penner, S. S. and Fuhs, A. E. (1957) On generalized scaling procedures for liquid-fuel rocket engines. Combustion and Flame, 1 (2). pp. 229-240. ISSN 0010-2180. http://resolver.caltech.edu/CaltechAUTHORS:20110118-105514911
- Published Version
Restricted to Repository administrators only
See Usage Policy.
Use this Persistent URL to link to this item: http://resolver.caltech.edu/CaltechAUTHORS:20110118-105514911
The scaling procedures of Penner and Tsien, of Crocco and of Barrère have been generalized by using the assumption that the mean drop size is proportional to the product of powers of the Weber number and the Reynolds number, together with the hypothesis that the total conversion time varies as a power (usually the second) of the drop diameter. The results obtained for the steady aero thermochemistry and for unstable motor operation (low-frequency and high-frequency oscillations) are shown to reduce to previously published rules when suitable simplifying assumptions are made.
|Additional Information:||© 1956 Elsevier. Received October 1956. Available online 8 August 2003. The work described in this paper was supported by the U.S. Air Force Office for Advanced Study, under Contract AF 18(603)-107 with the American Machine and Foundry Co. and Jet Propulsion Research. Inc.|
|Group:||Guggenheim Jet Propulsion Center|
|Other Numbering System:|
|Official Citation:||S.S. Penner, A.E. Fuhs, On generalized scaling procedures for liquid-fuel rocket engines, Combustion and Flame, Volume 1, Issue 2, June 1957, Pages 229-240, ISSN 0010-2180, DOI: 10.1016/0010-2180(57)90049-4. (http://www.sciencedirect.com/science/article/B6V2B-497YVN6-HY/2/0d90704982d27bcf58f74e62c387cdcc)|
|Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||Ruth Sustaita|
|Deposited On:||18 Jan 2011 19:30|
|Last Modified:||26 Dec 2012 12:51|
Repository Staff Only: item control page