Published June 1997
| public
Journal Article
Efficient high-pressure state equations
Chicago
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Abstract
A method is presented for a relatively accurate, noniterative, computationally efficient calculation of high-pressure fluid-mixture equations of state, especially targeted to gas turbines and rocket engines. Pressures above 1 bar and temperatures above 100 K are addressed. The method is based on curve fitting an effective reference state relative to departure functions formed using the Peng-Robinson cubic state equation. Fit parameters for H_2, O_2, N_2, propane, methane, n-heptane, and methanol are given.
Additional Information
© 1997 American Institute of Chemical Engineers. Issue online: 17 June 2004; Version of record online: 17 June 2004; Manuscript Revised: 10 January 1997; Manuscript Received: 2 May 1996. This research was conducted at the Jet Propulsion Laboratory and was sponsored by the NASA Marshall Space Flight Center with Mr. Klaus Gross as contract monitor, and by the NASA Lewis Research Center with Dr. Dan Bulzan as contract monitorAdditional details
- Eprint ID
- 82627
- Resolver ID
- CaltechAUTHORS:20171024-144448068
- NASA/JPL
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2017-10-24Created from EPrint's datestamp field
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2021-11-15Created from EPrint's last_modified field