Published March 1953
| Published
Journal Article
Open
On Maximum Evaporation Rates of Liquid Droplets in Rocket Motors
- Creators
- Penner, S. S.
Abstract
Upper limits have been estimated for the rate of evaporation of small liquid droplets in representative rocket combustion chambers. The droplets are assumed to be isothermal at all times. The droplet temperature as a function of time is determined by an appropriate heat balance. The calculations are useful in determining the significance of inelastic collisions between liquid droplets for complete combustion. Radiant heat transfer to moving liquid droplets is considered briefly.
Additional Information
Copyright 1953 American Rocket Society. Received July 14, 1952. This paper presents the results of one phase of research carried out at the Jet Propulsion Laboratory, California Institute of Technology, under U. S. Army Ordnance Department Contract No. W-04-200-ORD-1482. The original manuscript was distributed as Progress Report No. 9-13 by the Jet Propulsion Laboratory in September 1947.Attached Files
Published - 313505.pdf
Files
313505.pdf
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Additional details
- Eprint ID
- 16985
- Resolver ID
- CaltechAUTHORS:20091215-123319557
- W-04-200-ORD-1482
- Army Ordnance Department
- Created
-
2009-12-15Created from EPrint's datestamp field
- Updated
-
2019-10-03Created from EPrint's last_modified field
- Caltech groups
- Guggenheim Jet Propulsion Center
- Other Numbering System Name
- Guggenheim Jet Propulsion Center
- Other Numbering System Identifier
- 38