Published 1962
| Published
Book Section - Chapter
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Perturbation analysis of one-dimensional heterogeneous flow in rocket nozzles
- Creators
- Rannie, W. D.
Chicago
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Abstract
A perturbation analysis of the velocity and temperature lags in two-phase flow in rocket nozzles is developed and applied to the calculation of specific impulse and other performance characteristics of nozzles of arbitrary shape. Within the limitations of the one-dimensional flow approximation, the analysis is valid for distributions of particle diameters that are in a practical range.
Additional Information
© 1962, Submitted for publication to the American Rocket Society, Jan. 3, 1962. w. D. RANNIE is Robert H. Goddard Professor of Jet Propulsion, Daniel and Florence Guggenheim Jet Propulsion Center, Kármán Laboratory of Fluid Mechanics and Jet Propulsion.Attached Files
Published - 130_Ranni_WD.pdf
Files
130_Ranni_WD.pdf
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Additional details
- Eprint ID
- 21849
- Resolver ID
- CaltechAUTHORS:20110121-101804833
- Created
-
2011-02-04Created 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
- 130