The wake source model of Parkinson and Jandali is extended to cover lifting separated flows past two dimensional13; bodies. As in the symmetrical drag case the flow separation13; points are the critical points of a conformal mapping from13; s complex plane in which sources In the wake create stagnation conditions at the critical points. Then the stagnation streamlines in the complex plane map to tangential separation streamlines in the physical plane, with separation occuring at the given base pressure. The latter is assumed constant and the flow inside the separation streamlines is ignored. The extension of the wake source model to the general lifting case involves the handling of two problems. First a mapping has to be found in which the ...
The present work was mainly concerned with the fundamental processes that occur on a two-dimensional...
A wake model for the free-streamline theory is proposed to treat the two-dimensional flow past an ob...
Lift–dominated pointed aircraft configurations are considered in the transonic range. To make the ap...
A potential flow model is given for lifting, two-dimensional separated flows past bodies. Flow outsi...
The thesis deals with some new applications of the wake source model, a two-dimensional incompressib...
Continuing the study carried out by Dr. W.W.H. Yeung, a former Ph.D. student in the department of Me...
Fins, wings, blades and sails can generate lift and drag in both attached and separated flow conditi...
A simple method of solution to the problem of two-dimensional separated flow around multiple-body ci...
An exact theoretical treatment of the influence of sources of fluid on and within two-dimensional ae...
A flow model for a Joukowsky airfoil with an inclined spoiler or split flap is constructed based on ...
At present, a number of theories exist for the calculation of lift on delta wings with leading edge ...
The objective of this paper is to present a simple inviscid model for separated flow past two or thr...
A theory is presented for the calculation of the pressure distribution and lift for arbitrary thick ...
It seems possible that, in supersonic flight, unconventional arrangements of wings and bodies may of...
When an object generates lift as a result of its motion through the air, it leaves a typical signatu...
The present work was mainly concerned with the fundamental processes that occur on a two-dimensional...
A wake model for the free-streamline theory is proposed to treat the two-dimensional flow past an ob...
Lift–dominated pointed aircraft configurations are considered in the transonic range. To make the ap...
A potential flow model is given for lifting, two-dimensional separated flows past bodies. Flow outsi...
The thesis deals with some new applications of the wake source model, a two-dimensional incompressib...
Continuing the study carried out by Dr. W.W.H. Yeung, a former Ph.D. student in the department of Me...
Fins, wings, blades and sails can generate lift and drag in both attached and separated flow conditi...
A simple method of solution to the problem of two-dimensional separated flow around multiple-body ci...
An exact theoretical treatment of the influence of sources of fluid on and within two-dimensional ae...
A flow model for a Joukowsky airfoil with an inclined spoiler or split flap is constructed based on ...
At present, a number of theories exist for the calculation of lift on delta wings with leading edge ...
The objective of this paper is to present a simple inviscid model for separated flow past two or thr...
A theory is presented for the calculation of the pressure distribution and lift for arbitrary thick ...
It seems possible that, in supersonic flight, unconventional arrangements of wings and bodies may of...
When an object generates lift as a result of its motion through the air, it leaves a typical signatu...
The present work was mainly concerned with the fundamental processes that occur on a two-dimensional...
A wake model for the free-streamline theory is proposed to treat the two-dimensional flow past an ob...
Lift–dominated pointed aircraft configurations are considered in the transonic range. To make the ap...