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 (Short Take-Off Vertical Landing) Propulsion System Volume Dynamics Approximations
1989
11 pages
Report
No indication
English
STOVL propulsion system volume dynamics approximations
Tema Archive | 1989
|STOVL propulsion system volume dynamics approximations
NTRS | 1989
|