Estabilidad de un buque ultra heavy lift carrier

Se plantea la posible demanda en un futuro del transporte de grandes plataformas petrolíferas semisumergibles de más de 70.000 t de peso, para perforaciones a más de 10.000 pies de profundidad. Estudia la estabilidad de buques Heavy Lift Carrier con mangas atípicas, capaces de transportar estas cargas, y en algunos casos sobresaliendo por sus amuras. Para esto se: 1. Estudia y genera posibles carenas, su compartimentación y lastre para la inmersión o emersión de la cubierta de intemperie, a más de 10 m de profundidad para tomar o dejar la carga, optimizando el proceso. 2. Analiza la estabilidad del buque tanto en inmersión/emersión y navegación, con máximas cargas y con altos centros de gravedad, y establece ábacos de estabilidad límite en función de los parámetros del buque. 3. Plantea la corrección de estabilidad excesiva del buque en condiciones de navegación para evitar las excesivas aceleraciones. Los resultados obtenidos aportan ábacos que permiten, en función de los parámetros carga a transportar (Zg max) - Peso Carga), elegir el buque más adecuado, capaz de efectuar la inmersión, emersión, y navegación, y plantea acciones futuras de investigación. ABSTRACT This work raises the potential demand in the future, to transport large semisubmersible oil rigs over 70,000 tonnes of weight for drilling to 10,000 feet deep. Study vessel stability Heavy Lift Carrier with atypical breadths capable of carrying these burdens, and in some cases standing out for their bows. 1. Examines possible hulls, their partitioning and ballast for immersion or emersion of the weather deck, more than 10 m deep to take –loading (lifting) - or leave (off- loading). 2. Analyzes the stability of the vessel both immersion / emersion and navigation, with maximum loads with high centers of gravity and stability limit states abacus according to the parameters of the ship. 3. Correction raises the stability of the ship over navigation to prevent excessive accelerations. The results allow, in terms of cargo transport parameters (Zg max) - Weight Load), choosing the most suitable vessel capable of carrying out the immersion, emersion, and navigation, and suggests future research activities.

Face Lift Surgery for Reconstructed Virtual Humans

We introduce an innovative, semi-automatic method to transform low resolution facial meshes into high definition ones, based on the tailoring of a generic, neutral human head model, designed by an artist, to fit the facial features of a specific person. To determine these facial features we need to select a set of "control points" (corners of eyes, lips, etc.) in at least two photographs of the subject's face. The neutral head mesh is then automatically reshaped according to the relation between the control points in the original subject's mesh through a set of transformation pyramids. The last step consists in merging both meshes and filling the gaps that appear in the previous process. This algorithm avoids the use of expensive and complicated technologies to obtain depth maps, which also need to be meshed later.

Lift devices in the flight of Archaeopteryx

Archaeopteryx has played a central role in the debates on the origins of avian (and dinosaurian) flight, even though as a flier it probably represents a relatively late stage in the beginnings of fl ight. We report on aerodynamic tests using a life-sized model of Archaeopteryx performing in a low turbulence wind tunnel. Our results indicate that tail deflection significantly decreased take-off velocity and power consumption, and that the first manual digit could have functioned as the structural precursor of the alula. Such results demonstrate that Archaeopteryx had already evolved high-lift devices, which are functional analogues of those present in today's birds.

Global Stability Analysis of a Compressible Turbulent Flow around a High-Lift Configuration

The purpose of this work is to analyze a complex high lift configuration for which significant regions of separated flow are present. Current state of the art methods have some diffculty to predict the origin and the progression of this separated flow when increasing the angle of attack. The mechanisms responsible for the maximum lift limit on multi-element wing con?gurations are not clear; this stability analysis could help to understand the physics behind the phenomenon and to find a relation between the flow separation and the instability onset. The methodology presented herein consists in the computation of a steady base flow solution based on a finite volume discretization and a proposal of the solution for a generalized eigenvalue problem corresponding to the perturbed and linearized problem. The eigenvalue problem has been solved with the Arnoldi iterative method, one of the Krylov subspace projection methods. The described methodology was applied to the NACA0012 test case in subsonic and in transonic conditions and, finally, for the first time to the authors knowledge, on an industrial multi-component geometry, such as the A310 airfoil, in order to identify low frequency instabilities related to the separation. One important conclusion is that for all the analyzed geometries, one unstable mode related to flow separation appears for an angle of attack greater than the one correspondent to the maximum lift coe?cient condition. Finally, an adjoint study was carried out in order to evaluate the receptivity and the structural sensitivity of the geometries, giving an indication of the domain region that could be modified resulting in the biggest change of the flowfield.

Operational assessment of Paralympics transit system: low-floor buses, lift-equipped buses, and signage.

Federal Transit Administration, Washington, D.C.

The LIFT: special needs transportation in Portland, Oregon. Interim report.

Urban Mass Transportation Administration, Washington, D.C.

St. Stephen Powerhouse fish lift, Cooper River Rediversion Project, South Carolina : hydraulic model investigation /

"March 1993."

Emergency oil lift program and related oil problems.

Hearings held Feb. 5 - Mar. 22, 1957.

Powered-lift aircraft technology /

Mode of access: Internet.

Greenes ghost havnting conie-catchers / Wherein is set down, the arte of humouring. The arte of carrying stones. Will. St. lift. Ia. Fost. law. Ned Bro. catch. and Blacke Robins kindnesse. With the conceits of Doctor Pinch-backe a notable makeshift. Ten times more pleasant then anything yet published of this matter ... London, Printed for R. Iackson and I. North, 1602.

Mode of access: Internet.

Drag due to lift of a not-so-slender configuration; application of theory.

"Contract no. AF 33(616)-2933."

Reduction of drag due to lift at supersonic speeds

"Aeronautical Research Laboratory, Contract no. AF 33(616)-2170, Project no. 1366."

The influence of two-dimensional stream shear on airfoil maximum lift,

"Project 9R-38-01-000, Task 902. Contract DA 44-177-TC-439. U. S. Army Transportation Research Command, Transportation Corps, Fort Eustis, Virginia."

Report on the multiphase flow of gas, oil, and water through vertical flow strings with application to the design of gas lift installations,

Cover title.

Rhodesian sanctions, should the United States lift them? : Hearing and markup before the Committee on Foreign Affairs and its Subcommittees on Africa and on International Organizations, House of Representatives, Ninety-sixth Congress, first session, on S. 2076, December 5 and 11, 1979.

Mode of access: Internet.