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- W2324571469 abstract "This paper presents an aerodynamic comparison of vertical fin placement for a vertical takeoff, horizontal landing Reusable Booster System concept. This analysis was conducted using the CART3D inviscid CFD solver. The three configurations analyzed are a wing tip mounted, split tail fuselage mounted, and a single vertical fuselage mounted. This comparison is down at a relevant flight speed for a reusable booster system during re-entry from a rocketback trajectory." @default.
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- W2324571469 date "2011-06-14" @default.
- W2324571469 modified "2023-10-05" @default.
- W2324571469 title "Aerodynamic Properties of Vertical Stabilizer Placement for a Reusable Booster System" @default.
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- W2324571469 doi "https://doi.org/10.2514/6.2011-7163" @default.
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