... validation of the transition models implemented in REX is performed for several 2- and 3-dimensional geometries of naval relevance. Standard tests with extensive available experimental data include flat plates in zero pressure gradient, an airfoil, and sickle wing. More complex test cases include...

... distribution beneath the wing. 1 6 2007 1 6 2007 2007. The Society of Naval Architects and Marine Engineers Reservoir Characterization airfoil wing-in-ground effect vehicle depression Froude number effect flight pressure distribution disturbance wig vehicle free surface chord...

... geometry. 1 9 1994 1 9 1994 1994. The Society of Naval Architects and Marine Engineers passenger transportation hydrofoil convergence geometry surface panel method airfoil ship research iteration body surface equation total potential boundary condition pressure...

... is the closest point to the undisturbed free surface, and if the (squared) Froude number based on the trailing-edge height is less than the water/air density ratio. 1 12 1984 1 12 1984 1984. The Society of Naval Architects and Marine Engineers airfoil extreme ground effect closest point...

... mainsail sail shape chord incidence configuration equation single sail airfoil coefficient stagnation point separation Journal of Ship Research, Vol. 28, No. 1, March 1984, pp. 11-17 Two-Dimensional Sails in Inviscid Flow P. S. Jackson 1 This paper develops a general method for two-dimensional...

...James W. White The pressure distribution over a subsonic airfoil experiencing massive separation is analyzed by a zonal modeling approach. Important physics are included in the mathematical description of each zone, and the zones are allowed to interact until convergence of the overall flow...

... theoretical model straight line lateral force airfoil ship research force distribution cross section vertical wall sway force Computation integration ship slender body coefficient integral equation equation Journal of Ship Research, Vol. 23, No. 4, Dec. 1979, pp. 284-296 Lateral Forces...

...Jerome H. Milgram Two-dimensional airfoil theory is developed for incompressible flow, for which most aspects of the solution are found in a "mapped plane." Although the airfoil contour has large slopes in the physical plane when the airfoil has a round leading edge, the slopes in the mapped plane...