Andere Kunden interessierten sich auch für
![Computational Fluid Dynamics Testing for Drag Reduction of an Aircraft Laser Turret]( "Computational Fluid Dynamics Testing for Drag Reduction of an Aircraft Laser Turret")
Computational Fluid Dynamics Testing for Drag Reduction of an Aircraft Laser Turret63,99 €![Wind Tunnel Analysis and Flight Test of a Wing Fence on A T-38]( "Wind Tunnel Analysis and Flight Test of a Wing Fence on A T-38")
Wind Tunnel Analysis and Flight Test of a Wing Fence on A T-3863,99 €![A Study in Drag Reduction of Close Formation Flight Accounting for Flight Control Trim Positions and Dissimilar Formations]( "A Study in Drag Reduction of Close Formation Flight Accounting for Flight Control Trim Positions and Dissimilar Formations")
A Study in Drag Reduction of Close Formation Flight Accounting for Flight Control Trim Positions and Dissimilar Formations60,99 €![An Analytical Study of T-38 Drag Reduction in Tight Formation Flight]( "An Analytical Study of T-38 Drag Reduction in Tight Formation Flight")
An Analytical Study of T-38 Drag Reduction in Tight Formation Flight63,99 €![Wind Tunnel Ivestigation of Joined Wing Configurations]( "Wind Tunnel Ivestigation of Joined Wing Configurations")
Wind Tunnel Ivestigation of Joined Wing Configurations60,99 €![A Wind Tunnel Investigation of Joined Wing Scissor Morphing]( "A Wind Tunnel Investigation of Joined Wing Scissor Morphing")
A Wind Tunnel Investigation of Joined Wing Scissor Morphing61,99 €![Performing Particle Image Velocimetry in a Supersonic Wind Tunnel Using Carbon Dioxide as the Seed Material]( "Performing Particle Image Velocimetry in a Supersonic Wind Tunnel Using Carbon Dioxide as the Seed Material")
Performing Particle Image Velocimetry in a Supersonic Wind Tunnel Using Carbon Dioxide as the Seed Material60,99 €
This study investigated the use of aft-mounted fairings and splitter plates to reduce the drag of a half-scale aircraft laser turret. Forces, moments, and pressure distributions were measured in the AFIT 1.5-m (5-ft) wind tunnel at Reynolds numbers between 3x105 and 9x105 based on the turret diameter. Oil traces indicated the nature of the flow near the surface of the unmodified turret and the surrounding area. Tufts placed on the turret, fairings, and splitter plates showed changes in separation regions when configurations were changed. The flow around the turret was characterized by dominant vortices shedding from the top of the turret and a large trailing wake of vorticity. Splitter plates were ineffective in reducing drag as a result of the strong flow over the top of the turret. A small fairing reduced baseline drag by 49% but was unable to produce attached flow near the turret.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.