In studying an ideal cycle relevant to aircraft propulsion, one can have a good insight into the relevant important parameters that give the performance parameters of a given system. For such a study, the following assumptions are usually taken:
Thermodynamic Ideal Cycle Analysis
Springer Aerospace Techn.
15.05.2012
60 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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