Abstract
In allusion to the aerodynamic lift difference between tank test model and full scale plane, a simulation method of lift to tank test model is put forward, and conduct model test on rough water at the model status with boundary layer control technology (BLC) and without BLC, and then we study the influence of aerodynamic lift on trim and heaving characteristic of the test model systematically, the results turn out to be that: the influence of aerodynamic on trim is affected by test velocity, at relatively low speed, this difference can be ignored, but at higher speed, the maximum trim value difference lies the range of 2%∼7%, and the wave length corresponding to the maximum value decreases. The influence of aerodynamic on heaving is affected by wave length, at relative shorter wave length, the heaving value decreases a little between the model with BLC and without BLC, this difference lies about 10%, but this difference increases to 15%∼40% at higher wave length.
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.
