The large deformation problem of the wing with high aspect ratio cannot be avoided due to the large bending moment and poor torsional stiffness. The wing design follows the following procedure; firstly, the design indexes of high aspect ratio wing are preliminarily formulated referring to some param...
In this paper the variational problem for the shape of a thin lifting surface of high hypersonic performance is formulated by using analytical expressions obtained in [7, 8]for the flow around a small-aspect-ratio wing at an angle of attack in the next approximation to the Newtonian theory. ...
Flow separation over the side-edge of the wing, a feat known as the cause of roll stall where roll moment no longer increases with angle of attack, is seen to be affected by both changes in aspect ratio as well as changes in... T Linehan,K Mohseni - Aiaa Aerospace Sciences Meeting ...
A Survey of Opening up of Public Procurements : an aspect of the integration of European Community market The elimination of the former barriers finished with the completion of the customs union in the Community at the end of 1960s. The curtailments or ... T Mori - 《Bulletin of Saitama ...
The flow over a planar low-aspect-ratio delta wing is considered in the strong viscous-inviscid interaction regime. The study is carried out for Newtonian passage to limit, when the adiabatic exponent tends to unity, while the Mach and Reynolds numbers increase without bound. For the flow over...
This article is part of a series on Fundamentals Of Aircraft Design. Previous Next Sweep Angle And Supersonic Flight Share Category Home / Aircraft Design / Fundamentals of Aircraft Design Tags Aspect Ratio Sweep Angle Wing Area Wing Span
Question_1: I will need to have y+=1 close to the walls of the building, how can I do it? I've already done a really coarse mesh to make an attempt and Fluent gives me values of the wall shear stress of ~0.03 Pa. I tought then just to apply the formula ...
Selecting a good aspect ratio is crucial for effective 2D diagrams. There are several aspect ratio selection methods for function plots and line charts, but only few can handle general, discrete diagrams such as 2D scatter plots. However, these methods either lack a perceptual foundation or heavil...
The effects of blade aspect ratio and taper ratio are analyzed, which shows that the cycloidal rotors with the same chord length have quite similar performance even though the blade aspect ratio varies from a very small value to a large one. By comparing the cycloidal rotors with different ...
of considering an inertially slender aircraft. Almost certainly the aircraft is intended to be capable of supersonic speeds, in which case for the lowest wave drag the designer is forced to use a low aspect ratio wing of the smallest thickness/chord ratio structurally possible and a fuselage of...