Wind Tunnel Testing for Drag Reduction of an Aircraft Laser Turret by Christopher Snyder

Wind Tunnel Testing for Drag Reduction of an Aircraft Laser Turret

Christopher Snyder

112 pages missing pub info (editions)

nonfiction education medium-paced
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Description

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 number...

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