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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>INTERACTION OF PROPELLER NOZZLE WITH STERN FRAME, AND EXPERIMENTAL DETERMINATION OF ITS STRESSED CONDITION</title>
      <link>https://trid.trb.org/View/73351</link>
      <description><![CDATA[A design methodology aimed at extending the service life of a propeller nozzle is discussed.  Experimental data on the stress transmission between propeller and stern are given, together with diagrams of the forces acting on the nozzle-stern arrangement, including: (a) the effect of the propeller nozzle on the upper and lower stern-stiffeners, (b) the longitudinal distributin of interaction forces, and (c) during reversal of the rudder-setting.  Continuous fillet welding of the nozzle assembly and strengthening of the welded joints of the internal casing are advocated. Order from: BSRA as No. 48,019.]]></description>
      <pubDate>Wed, 14 Jun 1978 00:00:00 GMT</pubDate>
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      <title>SIMPLIFIED STERN BEARING INSPECTION</title>
      <link>https://trid.trb.org/View/1049</link>
      <description><![CDATA[Turnbull Marine Design Co., of Sale, Cheshire, England, has introduced a stern bearing which meets the special requirements for a new generation of superships, enabling any part of a tailshaft bearing or gland seal to be examined ( and replaced if necessary ) while the ship is afloat and at loaded draft.  The inboard end of the tailshaft has an integral solid forged coupling flange which is dimensioned to pass through the opening in the stern frame when the bearing has been removed.  Using an inflatable gland seal from inside the vessel, it is possible to service or renew any part of the outboard gland seal from inside the vessel.  The propeller is flange mounted and secured by hydraulically stressed bolts, thus eliminating the conventional taper mounting of the propeller.  The procedure for dismantling and examining the bearing is given.]]></description>
      <pubDate>Tue, 30 Oct 1973 00:00:00 GMT</pubDate>
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