Experimental study of the effect of helical grooves on an infinite cylinder
Approved for public release; distribution is unlimited === A series of low-speed wind-tunnel investigation were conducted to determine the aerodynamic behavior of a grooved cylinder representing a long trailing wire antenna towed from an orbiting airplane. The large angle-of-attack range of the tra...
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| Language: | en_US |
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Monterey, California. Naval Postgraduate School
2012
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| Online Access: | http://hdl.handle.net/10945/23893 |