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The study focuses on aerodynamic improvements for a half-scale aircraft laser turret by exploring aft-mounted fairings and splitter plates to minimize drag. Conducted in a wind tunnel, it measured various aerodynamic forces and pressure distributions at specific Reynolds numbers. Observations included flow characteristics, with dominant vortices and trailing wakes identified. While splitter plates proved ineffective, a small fairing significantly reduced drag by 49%, although it failed to maintain attached flow near the turret, highlighting the complexities of aerodynamic design.
Buchkauf
Wind Tunnel Testing for Drag Reduction of an Aircraft Laser Turret, Christopher Snyder
- Sprache
- Erscheinungsdatum
- 2012
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- Titel
- Wind Tunnel Testing for Drag Reduction of an Aircraft Laser Turret
- Sprache
- Englisch
- Autor*innen
- Christopher Snyder
- Verlag
- 2012
- Einband
- Paperback
- Seitenzahl
- 112
- ISBN13
- 9781288369058
- Kategorie
- Pädagogik
- Beschreibung
- The study focuses on aerodynamic improvements for a half-scale aircraft laser turret by exploring aft-mounted fairings and splitter plates to minimize drag. Conducted in a wind tunnel, it measured various aerodynamic forces and pressure distributions at specific Reynolds numbers. Observations included flow characteristics, with dominant vortices and trailing wakes identified. While splitter plates proved ineffective, a small fairing significantly reduced drag by 49%, although it failed to maintain attached flow near the turret, highlighting the complexities of aerodynamic design.