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
1989-01-01
Conference paper
No indication
English
STOVL propulsion system volume dynamics approximations
Tema Archive | 1989
|NASA supersonic STOVL propulsion technology program
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AIAA | 1989
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