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- W2005351545 abstract "The generation of significant side forces and yawing moments on an F/A-18 fuselage through tangential slot blowing is analyzed using computational fluid dynamics. The effects of freestream Mach number, jet exit conditions, jet length, and jet location are studied. The effects of over- and underblowing on force and moment production are analyzed. Non-time-accurate solutions are obtained to determine the steady-state side forces, yawing moments, and surface pressure distributions generated by tangential slot blowing. Time-accurate solutions are obtained to study the force onset time lag of tangential slot blowing. Comparison with available experimental data from full-scale wind-tunnel and subscale wind-tunnel tests are made. This computational analysis complements the experimental results and provides a detailed understanding of the effects of tangential slot blowing on the flowfield about the isolated F/A-18 forebody. Additionally, it extends the slot-blowing database to transonic maneuvering Mach numbers." @default.
- W2005351545 created "2016-06-24" @default.
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- W2005351545 date "1994-06-20" @default.
- W2005351545 modified "2023-09-23" @default.
- W2005351545 title "Analysis of tangential slot blowing on F/A-18 isolated forebody" @default.
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- W2005351545 doi "https://doi.org/10.2514/6.1994-1831" @default.
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