Tank Tests To Determine The Effect Of Varying Design Parameters Of Planing Tail Hulls
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Tank Tests to Determine the Effect of Varying Design Parameters of Planing-tail Hulls
The second part of a series of tests made in Langley tank no. 2 to determine the effect of varying design parameters of planing-tail hulls is presented. Results are given to show the effects on resistance characteristics of varying angle of afterbody keel, depth of step, and length of afterbody chine. The effect of varying the gross load is shown for one configuration. The resistance characteristics of planing-tail hulls are compared withthose of a conventional flying-boat hull. The forces on the forebody and afterbody of one configuration are compared with the forces on a conventional hull.
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1949
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1952