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Finite Element Analysis of Transonic Flows Over Thin Airfoils

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Release : 1976
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Book Synopsis Finite Element Analysis of Transonic Flows Over Thin Airfoils by : S. T. K. Chan

Download or read book Finite Element Analysis of Transonic Flows Over Thin Airfoils written by S. T. K. Chan. This book was released on 1976. Available in PDF, EPUB and Kindle. Book excerpt: A finite element algorithm is described for computing steady and unsteady (oscillatory and transient) transonic flows over thin airfoils by solving directly the unsteady, nonlinear transonic potential equation based on small disturbance theory. The numerical algorithm is developed using the concept of finite elements in conjunction with the least squares method of weighted residuals applied to both space and time. The basic element presently used is a product of an element in space and an element in time. The former has a cubic expansion inside each element, while the latter is a quadratic Lagrange element. The embedded shocks are smeared and, in computing flow over lifting airfoils, use is made of the far field asymptotic solution to increase computational efficiency. For each time step, the finite element discretization in both space and time results in a recurrence relationship in the form of a banded system of algebraic equations, which is solved by Gaussian eliminations. Sample problems of steady flow over lifting airfoils and unsteady flow over airfoils executing harmonic motion are calculated to demonstrate the applicability and validity of the present approach. The solution procedures are found to be adequately accurate and very efficient, with unsteady solution obtainable in less than ten minutes CPU time on a CDC 6600 computer. (Author).

Finite Element Analysis of Transonic Flows Over Thin Airfoils. Volume II. Program User's Manual

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Release : 1976
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Book Synopsis Finite Element Analysis of Transonic Flows Over Thin Airfoils. Volume II. Program User's Manual by : H. C. Chen

Download or read book Finite Element Analysis of Transonic Flows Over Thin Airfoils. Volume II. Program User's Manual written by H. C. Chen. This book was released on 1976. Available in PDF, EPUB and Kindle. Book excerpt: A finite element program is described for computing steady and unsteady (oscillatory and transient) transonic flows over thin airfoils by solving directly the unsteady, nonlinear transonic potential equation based on small disturbance theory. The present numerical algorithm is developed using the concept of finite elements in conjunction with the least squares method of weighted residuals applied to both space and time. The basic element presently used is a product of an element in space and an element in time. The former has a cubic expansion inside each element, while the latter is a quadratic Lagrangian element. For each time step, the finite element discretization in both space and time results in a recurrence relationship in the form of a banded system of algebraic equations, which is solved by Gaussian elimination. The embedded shocks are smeared and a matching scheme for computing effectively flow over lifting airfoils is also incorporated in the program. The present computer program is composed of two parts: the first part (designated as UTRANL-I) generates, from a limited number of input cards, the necessary mesh information and, if desired, produces a CALCOMP mesh plot; the second part (UTRANL-II) carries out the analysis and displays the pressure coefficients along the chordline on printer plots. Two sample cases of flow over a NACA 64A 410 and a NACA 64A 006 airfoils are given to demonstrate the applicability and usage of the program. Te solution procedures are found to be quite efficient and accurate, permitting the aerodynamic forces to be calculated to engineering accuracy in less than ten minutes CPU time on a CDC 6600 computer for the most time consuming case among all those studied. (Author).

Computer Program for Steady Transonic Flow Over Thin Airfoils by Finite Elements

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Release : 1975
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Book Synopsis Computer Program for Steady Transonic Flow Over Thin Airfoils by Finite Elements by : S. T. K. Chan

Download or read book Computer Program for Steady Transonic Flow Over Thin Airfoils by Finite Elements written by S. T. K. Chan. This book was released on 1975. Available in PDF, EPUB and Kindle. Book excerpt: A finite element program is described for the analysis of subsonic and transonic flows over thin airfoils by solving the nonlinear transonic potential equation based on small disturbance theory. The present numerical algorithm uses the concept of finite elements in conjunction with the least square method of weighted residuals. Since the governing equation is of the elliptic-hyperbolic type, a 'one-sided assembly technique' was devised and adapted in the supersonic region to restore the directional property of the flow, which was removed by the exclusion of entropy from the transonic potential equation. The finite element discretization results in a system of banded nonlinear algebraic equations, which is solved by direct iterations. The elements presently used include triangles and quadrilaterals with the perturbed potential function and velocity components as nodal unknowns. Boundary conditions of both Dirichlet and Neumann types are therefore imposed conveniently. Secondary unknowns are computed directly without resorting to numerical differentiation. The computer program is separated into two parts: the first part (designated as STRANL-I) generates the necessary mesh information and, if desired, produces a mesh plot and optimal nodal numbering as well; STRANL-II carries out the analysis and displays the pressure coefficients along the chord line on printer plots. Two sample cases of flow over a NACA 64 A006 and a 6% thick circular arc are given.

Investigation of Upwind Schemes for Finite Element Analysis of Transonic Flow Over Thin Airfoils

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Release : 1981
Genre : Aerodynamics, Transonic
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Book Synopsis Investigation of Upwind Schemes for Finite Element Analysis of Transonic Flow Over Thin Airfoils by : Dennis L. Hunt (2LT, USAF.)

Download or read book Investigation of Upwind Schemes for Finite Element Analysis of Transonic Flow Over Thin Airfoils written by Dennis L. Hunt (2LT, USAF.). This book was released on 1981. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of Upwind Schemes for Finite Element Analysis of Transonic Flow Over Thin Airfoils

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Release : 1981
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Book Synopsis Investigation of Upwind Schemes for Finite Element Analysis of Transonic Flow Over Thin Airfoils by : Dennis L. Hunt

Download or read book Investigation of Upwind Schemes for Finite Element Analysis of Transonic Flow Over Thin Airfoils written by Dennis L. Hunt. This book was released on 1981. Available in PDF, EPUB and Kindle. Book excerpt: Two finite element upwind techniques were investigated to see if convergent solutions could be obtained from the transonic potential equation for steady flow over thin airfoils. The first technique involves the use of parabolic upwind functions, that when added to the shape functions weight the upstream node in the supersonic region more than the downwind nodes. The second technique integrates the finite element equations over the area that influences the solution (i.e., the area inside a mach cone). (Author).

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