Two approaches to modeling turbofan engine component volume dynamics are explored and compared with a view toward application to real-time simulation of short take-off vertical landing (STOVL) aircraft propulsion systems. The first (and most popular) approach considers only heat and mass balances; the second approach includes a momentum balance and substitutes the heat equation with a complete energy balance. Results for a practical test case are presented and discussed.
STOVL propulsion system volume dynamics approximations
1989 Winter Annual Meeting ; 1989 ; San Francisco, CA, United States
01.01.1989
Aufsatz (Konferenz)
Keine Angabe
Englisch
STOVL propulsion system volume dynamics approximations
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