Seymour, Ernest Richard (1962) Some investigations of heterogeneous flow in a rocket nozzle. Engineer's thesis, California Institute of Technology. http://resolver.caltech.edu/CaltechETD:etd-12072005-133112
In the heterogeneous flow of finely divided particles and gas in a rocket nozzle, the assumptions that the flow enters the nozzle with no lags, that the radiative transport of energy between particles is negligible, and that there are no temperature gradients within the particles, are commonly made. In this paper, each of these assumptions is investigated in detail, and they are shown to be reasonable for typical rocket nozzles.
|Item Type:||Thesis (Engineer's thesis)|
|Degree Grantor:||California Institute of Technology|
|Division:||Engineering and Applied Science|
|Thesis Availability:||Public (worldwide access)|
|Defense Date:||1 January 1962|
|Default Usage Policy:||No commercial reproduction, distribution, display or performance rights in this work are provided.|
|Deposited By:||Imported from ETD-db|
|Deposited On:||08 Dec 2005|
|Last Modified:||26 Dec 2012 03:12|
- Final Version
See Usage Policy.
Repository Staff Only: item control page