Publication Date:
2022-06-16
Description:
After almost exclusive use in oceanographic research, the R. V. "Meteor" conducted tests in fall 1967 in the Baltic Sea which were devoted to an important problem in ship building research. In order to check the transfer of model test results to prototype conditions, which has become somewhat uncertain in view of the increase in size and speed of modern vessels, a model family of this ship had been tested at scales of 1: 25, 1 : 19 and 1 : 13 .7 5, and full scale tests were to complete the series. The most important measurements included resistance, propeller thrust and propeller power demand. Furthermore, the nomial wake in the absence of the propeller and the effective wake in front of the working propeller, the velocity distribution in the boundary layer at one point of the hull at least and the behaviour of the ship during manoeuvering with and without propeller have been investigated. The most difficult task consisted of the determination of the resistance as a function of speed, because the ship could not be driven by propeller for these tests, but had to be moved, similar to a model on a towing carriage, by a known force exerted above the water surface. Following the historical example of the resistance tests on the ferry boat "Lucy Ashton", the "Meteor" was supplied with 3 jets, which, with a maximum thrust of about 10 Mp at 12 OOO PS, produced a forward speed of 12 kn (Fig. 1, i., 3). The jet thrust was measured by strain gauges on the diagonals in the supporting frame of each jet (Fig. 3). Measurements of thrust and torque of the propeller were also obtained from strain gauges on the propeller shaft (Fig. 7). Wake measurements were performed with pitot tubes and a total head tube fixed on a rake (Fig. 4) which could be turned by 180° on the stem tube. Boundary layer measurements were obtained by two Prandtl tubes which could be moved sideways at the hull (Fig. 6). Rudder forces were indicated by a three component balance on the rudder shaft. Ott current meters and Prandtl tubes, calibrated on the mile distance, gave the ship speed. All measurements were performed electronically with analog and digital registration. The results obtained so far are remarkably accurate. Plotting the resistance values in the system of the model family indicates, that the ITTC 1957 line, presently in use as an extrapolator for frictional resistance, has too small a slope (Fig. 11 ). The total efficiency of model and prototype is about equal (Fig. 14), and the thrust deduction fraction does not seem to depend on the scale either. For the law of the wall of the boundary layer, the values K = 0.41 and C = 5.0 from recent laboratory tests are supported (Fig. 15). The evaluation of all results will probably be finished by the end of 1968.
Type:
Article
,
PeerReviewed
Format:
text
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