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Users manual for program NYQUIST: Liquid rocket nyquist plots developed for use on a PC computerThe 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 NYQUIST code. The capability to modify the input on line has been implemented. The configurations allowed include multiple tanks, multiple engines, and the splitting of a pipe into unequal 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. The code is too large to compile as one program using Microsoft FORTRAN 5; therefore, the code was broken into two segments: NYQUIST1.FOR and NYQUIST2.FOR. These are compiled separately and then linked together. The final run code is not too large (approximately equals 344,000 bytes).
Document ID
19930003334
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Armstrong, Wilbur C.
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:184451
NASA-CR-184451
Report Number: NAS 1.26:184451
Report Number: NASA-CR-184451
Accession Number
93N12522
Funding Number(s)
CONTRACT_GRANT: NAS8-36955
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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