Actions for Users manual for program SSFREQ intermediate mode stability curves : Developed for use on a PC computer

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Users manual for program SSFREQ intermediate mode stability curves : Developed for use on a PC computer

Author
Armstrong, Wilbur C.
Published
Jun 1, 1992.
Physical Description
1 electronic document
Online Version

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
The piping in a liquid rocket can assume complex configurations due to multiple tanks, multiple engines, and structures that must be piped around. The capability to handle some of these complex configurations have been incorporated into the SSFREQ code. The capability to modify the input on line has been implemented. The configurations allowed include multiple tanks, multiple engines, the splitting of a pipe into equal segments going to different (or the same) engines. This program will handle the following type elements: straight pipes, bends, inline accumulators, tuned stub accumulators, Helmholtz resonators, parallel resonators, pumps, split pipes, multiple tanks, and multiple engines.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19930003487.
Accession ID: 93N12675.
NAS 1.26:184452.
NASA-CR-184452.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15673916