Add to ORKGA problem of determining a shape of the airfoil being streamlined by a potential incompressible inviscid flow is solved by the successive approximation method using a specified chord velocity diagram. It is shown that a closed airfoil that possesses a specified chord velocity diagram can be constructed with a sufficient accuracy; if the chord diagram is unsuccessfully specified, the closed airfoil may prove to be not univalent, that is, physically unrealizable. © 2009 Allerton Press, Inc
A theory is developed for the airfoil of finite span at supersonic speed analogous to the Prandtl ai...
it was noted in the article, that initially the problem of interpolation of the simple plane curve a...
A New method for designing Natural Laminar Airfoils is13; described. It is based on three ideas: Fir...
A problem of determining a shape of the airfoil being streamlined by a potential incompressible invi...
By the assumption that the pressure-volume relation is linear, a method is given for computing the a...
The study deals with wing profiles in an ideal incompressible fluid and subsonic flow of an ideal ga...
An exact solution of the problem of designing an airfoil with a prescribed velocity distribution on ...
Title: Solution of inverse problem for a flow around an airfoil Author: Mgr. Jan Šimák Department: D...
An airfoil design technique is described which uses an analytical method for representing the airfoi...
This study examines an advanced viscous-inviscid interactive method developed for the analysis and d...
In this method the inviscid flow field is decomposed into two parts: a known field with constant vor...
An exact solution of the problem of designing an airfoil with a prescribed velocity distribution on ...
The problem is solved of designing a symmetric airfoil with upstream blowing opposite to subsonic ir...
An iteration method for airfoil shape completing using the pressure coefficient distribution specifi...
An airfoil design procedure, applicable to both subcritical and supercritical airfoils, is described...
A theory is developed for the airfoil of finite span at supersonic speed analogous to the Prandtl ai...
it was noted in the article, that initially the problem of interpolation of the simple plane curve a...
A New method for designing Natural Laminar Airfoils is13; described. It is based on three ideas: Fir...
A problem of determining a shape of the airfoil being streamlined by a potential incompressible invi...
By the assumption that the pressure-volume relation is linear, a method is given for computing the a...
The study deals with wing profiles in an ideal incompressible fluid and subsonic flow of an ideal ga...
An exact solution of the problem of designing an airfoil with a prescribed velocity distribution on ...
Title: Solution of inverse problem for a flow around an airfoil Author: Mgr. Jan Šimák Department: D...
An airfoil design technique is described which uses an analytical method for representing the airfoi...
This study examines an advanced viscous-inviscid interactive method developed for the analysis and d...
In this method the inviscid flow field is decomposed into two parts: a known field with constant vor...
An exact solution of the problem of designing an airfoil with a prescribed velocity distribution on ...
The problem is solved of designing a symmetric airfoil with upstream blowing opposite to subsonic ir...
An iteration method for airfoil shape completing using the pressure coefficient distribution specifi...
An airfoil design procedure, applicable to both subcritical and supercritical airfoils, is described...
A theory is developed for the airfoil of finite span at supersonic speed analogous to the Prandtl ai...
it was noted in the article, that initially the problem of interpolation of the simple plane curve a...
A New method for designing Natural Laminar Airfoils is13; described. It is based on three ideas: Fir...