Abstract
An infinite-Froude-number, or aerodynamic, theory is developed for the prediction of the additional lift, drag, moment and flap-hinge moment acting on a planing vessel fitted with transom-stern flapsExcellent agreement between the theory and the experiment for lift, drag and flap-hinge moment is obtained for flap-chord-to-vessel-beam ratios of 0.1 and 0.2. However, the theory slightly underpredicts the experimental data for greater values of the flap chord.The predictions for the moment are much less satisfactory. It is therefore recommended to repeat the experiments using modern instrumentation.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
