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    <title>Transport Research International Documentation (TRID)</title>
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    <copyright>Copyright © 2026. National Academy of Sciences. All rights reserved.</copyright>
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    <managingEditor>tris-trb@nas.edu (Bill McLeod)</managingEditor>
    <webMaster>tris-trb@nas.edu (Bill McLeod)</webMaster>
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      <title>ASSESSMENT OF THE PROPELLER TUNNELS ON THE COAST GUARD'S HERITAGE CLASS PATROL BOAT</title>
      <link>https://trid.trb.org/View/406044</link>
      <description><![CDATA[The purpose of the study is to examine flow characteristics through the propeller tunnel of the Coast Guard's Heritage Class Patrol Boat. Of particular interest is the possibility of separation along the tunnel roof, and pressure recovery at the tunnel exit. Two tunnel configurations were examined and compared. Results indicate that separation is highly unlikely at the tunnel entrance for both a rounded entrance and square entrance configuration. Pressure recovery characteristics for the square entrance tunnel with a downward exit slope proved to be more favorable than the rounded tunnel. Findings of the study are in agreement with cited literature.]]></description>
      <pubDate>Mon, 03 Oct 1994 00:00:00 GMT</pubDate>
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      <title>THE AERODYNAMIC CHARACTERISTICS OF A VEHICLE TRAVELING IN A TUNNEL OF FINITE LENGTH</title>
      <link>https://trid.trb.org/View/6325</link>
      <description><![CDATA[The experimental study investigates the dependence of the drag coefficient of a vehicle, moving coaxially with uniform linear velocity through a solid wall tube of finite length, on the ratio of the relative velocity of the induced fluid pushed ahead of the vehicle to the absolute velocity of the vehicle.  An apparatus was built with a vertical acrylic test tube, 25 ft. high and 1.732 in. inside diameter.  The tube was provided with water flow of different negative and positive pressure gradients.  Drop tests were conducted using models with smooth surface, in the form of cylinders with a streamlined nose and conical tail.  The mode of variation of the drag coefficient with the velocity ratio at model Reynolds number of 100,000 was experimentally established for the test parameters.  (Author)]]></description>
      <pubDate>Fri, 24 Nov 1972 00:00:00 GMT</pubDate>
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