Jameson, Antony 1934
Overview
Works:  71 works in 97 publications in 1 language and 1,537 library holdings 

Genres:  Conference proceedings 
Roles:  Author, Thesis advisor, Honoree, Editor 
Classifications:  QA3, 629.13432 
Publication Timeline
.
Most widely held works about
Antony Jameson
Most widely held works by
Antony Jameson
Aerodynamic design via control theory
by
Antony Jameson(
)
3 editions published in 1988 in English and held by 268 WorldCat member libraries worldwide
3 editions published in 1988 in English and held by 268 WorldCat member libraries worldwide
Frontiers of computational fluid dynamics 1994
(
Book
)
4 editions published between 1994 and 1995 in English and held by 170 WorldCat member libraries worldwide
4 editions published between 1994 and 1995 in English and held by 170 WorldCat member libraries worldwide
Essential elements of computational algorithms for aerodynamic analysis and design under contracts NAS197046 & NAS119480
by
Antony Jameson(
Book
)
2 editions published in 1997 in English and held by 78 WorldCat member libraries worldwide
2 editions published in 1997 in English and held by 78 WorldCat member libraries worldwide
Control theory based airfoil design for potential flow and a finite volume discretization
by J Reuther(
Book
)
1 edition published in 1995 in English and held by 76 WorldCat member libraries worldwide
1 edition published in 1995 in English and held by 76 WorldCat member libraries worldwide
Analysis and design of numerical schemes for gas dynamics 2 artificial diffusion, discrete shock structure
by
Antony Jameson(
Book
)
2 editions published in 1994 in English and held by 73 WorldCat member libraries worldwide
Abstract: "The effect of artificial diffusion on discrete shock structures is examined for a family of schemes which includes scalar diffusion, convective upwind and split pressure (CUSP) schemes, and upwind schemes with characteristic splitting. The analysis leads to conditions on the diffusive flux such that stationary discrete shocks can contain a single interior point. The simplest formulation which meets these conditions is a CUSP scheme in which the coefficients of the pressure differences is fully determined by the coefficient of convective diffusion. It is also shown how both the characteristic and CUSP schemes can be modified to preserve constant stagnation enthalpy in steady flow, leading to four variants, the E and Hcharacteristic schemes, and the E and HCUSP schemes. Numerical results are presented which confirm the properties of these schemes."
2 editions published in 1994 in English and held by 73 WorldCat member libraries worldwide
Abstract: "The effect of artificial diffusion on discrete shock structures is examined for a family of schemes which includes scalar diffusion, convective upwind and split pressure (CUSP) schemes, and upwind schemes with characteristic splitting. The analysis leads to conditions on the diffusive flux such that stationary discrete shocks can contain a single interior point. The simplest formulation which meets these conditions is a CUSP scheme in which the coefficients of the pressure differences is fully determined by the coefficient of convective diffusion. It is also shown how both the characteristic and CUSP schemes can be modified to preserve constant stagnation enthalpy in steady flow, leading to four variants, the E and Hcharacteristic schemes, and the E and HCUSP schemes. Numerical results are presented which confirm the properties of these schemes."
Optimum aerodynamic design via boundary control
by
Antony Jameson(
Book
)
2 editions published in 1994 in English and held by 72 WorldCat member libraries worldwide
Abstract: "These lectures describe the implementation of optimization techniques based on control theory for airfoil and wing design. In previous studies [10,11] it was shown that control theory could be used to devise an effective optimization procedure for twodimensional profiles in which the shape is determined by a conformal transformation from a unit circle, and the control is the mapping function. Recently the method has been implemented in an alternative formulation which does not depend on conformal mapping, so that it can more easily be extended to treat general configurations [16]. The method has also been extended to treat the Euler equations, and results are presented for both two and three dimensional cases, including the optimization of a swept wing."
2 editions published in 1994 in English and held by 72 WorldCat member libraries worldwide
Abstract: "These lectures describe the implementation of optimization techniques based on control theory for airfoil and wing design. In previous studies [10,11] it was shown that control theory could be used to devise an effective optimization procedure for twodimensional profiles in which the shape is determined by a conformal transformation from a unit circle, and the control is the mapping function. Recently the method has been implemented in an alternative formulation which does not depend on conformal mapping, so that it can more easily be extended to treat general configurations [16]. The method has also been extended to treat the Euler equations, and results are presented for both two and three dimensional cases, including the optimization of a swept wing."
Analysis and design of numerical schemes for gas dynamics 1 artificial diffusion, upwind biasing, limiters and their effect on accuracy and multigrid convergence
by
Antony Jameson(
Book
)
2 editions published in 1994 in English and held by 72 WorldCat member libraries worldwide
Abstract: "The theory of nonoscillatory scalar schemes is developed in this paper in terms of the local extremum diminishing (LED) principle that maxima should not increase and minima should not decrease. This principle can be used for multidimensional problems on both structured and unstructured meshes, while it is equivalent to the total variation diminishing (TVD) principle for onedimensional problems. A new formulation of symmetric limited positive (SLIP) schemes is presented, which can be generalized to produce schemes with arbitrary high order of accuracy in regions where the solution contains no extrema, and which can also be implemented on multidimensional unstructured meshes. Systems of equations lead to waves traveling with distinct speeds and possibly in opposite directions. Alternative treatments using characteristic splitting and scalar diffusive fluxes are examined, together with a modification of the scalar diffusion through the addition of pressure differences to the momentum equations to produce full upwinding in supersonic flow. This convective upwind and split pressure (CUSP) scheme exhibits very rapid convergence in multigrid calculations of transonic flow, and provides excellent shock resolution at very high Mach numbers."
2 editions published in 1994 in English and held by 72 WorldCat member libraries worldwide
Abstract: "The theory of nonoscillatory scalar schemes is developed in this paper in terms of the local extremum diminishing (LED) principle that maxima should not increase and minima should not decrease. This principle can be used for multidimensional problems on both structured and unstructured meshes, while it is equivalent to the total variation diminishing (TVD) principle for onedimensional problems. A new formulation of symmetric limited positive (SLIP) schemes is presented, which can be generalized to produce schemes with arbitrary high order of accuracy in regions where the solution contains no extrema, and which can also be implemented on multidimensional unstructured meshes. Systems of equations lead to waves traveling with distinct speeds and possibly in opposite directions. Alternative treatments using characteristic splitting and scalar diffusive fluxes are examined, together with a modification of the scalar diffusion through the addition of pressure differences to the momentum equations to produce full upwinding in supersonic flow. This convective upwind and split pressure (CUSP) scheme exhibits very rapid convergence in multigrid calculations of transonic flow, and provides excellent shock resolution at very high Mach numbers."
A comparison of design variables for control theory based airfoil optimization
by James Reuther(
Book
)
2 editions published in 1995 in English and held by 72 WorldCat member libraries worldwide
2 editions published in 1995 in English and held by 72 WorldCat member libraries worldwide
Supersonic wing and wingbody shape optimization using an adjoint formulation
by James Reuther(
Book
)
2 editions published in 1995 in English and held by 72 WorldCat member libraries worldwide
Abstract: "This paper describes the implementation of optimization techniques based on control theory for wing and wingbody design of supersonic configurations. The work represents an extension of our earlier research in which control theory is used to devise a design procedure that significantly reduces the computational cost by employing an adjoint equation. In previous studies it was shown that control theory could be used to devise transonic design methods for airfoils and wings in which the shape and the surrounding bodyfitted mesh are both generated analytically, and the control is the mapping function [5, 6, 8]. The method has also been implemented for both transonic potential flows and transonic flows governed by the Euler equations using an alternative formulation which employs numerically generated grids, so that it can treat more general configurations [16, 9, 17]. Here results are presented for threedimensional design cases subject to supersonic flows governed by the Euler equation."
2 editions published in 1995 in English and held by 72 WorldCat member libraries worldwide
Abstract: "This paper describes the implementation of optimization techniques based on control theory for wing and wingbody design of supersonic configurations. The work represents an extension of our earlier research in which control theory is used to devise a design procedure that significantly reduces the computational cost by employing an adjoint equation. In previous studies it was shown that control theory could be used to devise transonic design methods for airfoils and wings in which the shape and the surrounding bodyfitted mesh are both generated analytically, and the control is the mapping function [5, 6, 8]. The method has also been implemented for both transonic potential flows and transonic flows governed by the Euler equations using an alternative formulation which employs numerically generated grids, so that it can treat more general configurations [16, 9, 17]. Here results are presented for threedimensional design cases subject to supersonic flows governed by the Euler equation."
Control theory based airfoil design using the Euler equations
by
Antony Jameson(
Book
)
2 editions published in 1994 in English and held by 71 WorldCat member libraries worldwide
Abstract: "This paper describes the implementation of optimization techniques based on control theory for airfoil design. In our previous work [9, 10, 15] it was shown that control theory could be employed to devise effective optimization procedures for twodimensional profiles by using the potential flow equation with either a conformal mapping or a general coordinate system. The goal of our present work is to extend the development to treat the Euler equations in twodimensions by procedures that can readily be generalized to treat complex shapes in threedimensions. Therefore, we have developed methods which can address airfoil design through either an analytic mapping or an arbitrary grid perturbation method applied to a finite volume discretization of the Euler equations. Here the control law serves to provide computationally inexpensive gradient information to a standard numerical optimization method. Results are presented for both the inverse problem and drag minimization problem."
2 editions published in 1994 in English and held by 71 WorldCat member libraries worldwide
Abstract: "This paper describes the implementation of optimization techniques based on control theory for airfoil design. In our previous work [9, 10, 15] it was shown that control theory could be employed to devise effective optimization procedures for twodimensional profiles by using the potential flow equation with either a conformal mapping or a general coordinate system. The goal of our present work is to extend the development to treat the Euler equations in twodimensions by procedures that can readily be generalized to treat complex shapes in threedimensions. Therefore, we have developed methods which can address airfoil design through either an analytic mapping or an arbitrary grid perturbation method applied to a finite volume discretization of the Euler equations. Here the control law serves to provide computationally inexpensive gradient information to a standard numerical optimization method. Results are presented for both the inverse problem and drag minimization problem."
Multigrid solution of the NavierStokes equations on triangular meshes
by
Dimitri J Mavriplis(
Book
)
1 edition published in 1989 in English and held by 67 WorldCat member libraries worldwide
1 edition published in 1989 in English and held by 67 WorldCat member libraries worldwide
Aerodynamic shape optimization of wing and wingbody configurations using control theory
by James Reuther(
Book
)
2 editions published in 1995 in English and held by 67 WorldCat member libraries worldwide
Abstract: "This paper describes the implementation of optimization techniques based on control theory for wing and wingbody design. In previous studies [18, 19, 22] it was shown that control theory could be used to devise an effective optimization procedure for airfoils and wings in which the shape and the surrounding bodyfitted mesh are both generated analytically, and the control is the mapping function. Recently, the method has been implemented for both potential flows and flows governed by the Euler equations using an alternative formulation which employs numerically generated grids, so that it can more easily be extended to treat general configurations [34, 23]. Here results are presented both for the optimization of a swept wing using an analytic mapping, and for the optimization of wing and wingbody configurations using a general mesh."
2 editions published in 1995 in English and held by 67 WorldCat member libraries worldwide
Abstract: "This paper describes the implementation of optimization techniques based on control theory for wing and wingbody design. In previous studies [18, 19, 22] it was shown that control theory could be used to devise an effective optimization procedure for airfoils and wings in which the shape and the surrounding bodyfitted mesh are both generated analytically, and the control is the mapping function. Recently, the method has been implemented for both potential flows and flows governed by the Euler equations using an alternative formulation which employs numerically generated grids, so that it can more easily be extended to treat general configurations [34, 23]. Here results are presented both for the optimization of a swept wing using an analytic mapping, and for the optimization of wing and wingbody configurations using a general mesh."
Highresolution shock capturing scheme for high Mach number internal flow
by
Seokkwan Yoon(
Book
)
1 edition published in 1986 in English and held by 66 WorldCat member libraries worldwide
1 edition published in 1986 in English and held by 66 WorldCat member libraries worldwide
Multigrid solution of the Euler equations on unstructured and adaptive meshes
by
Dimitri Mavriplis(
Book
)
2 editions published in 1987 in English and held by 66 WorldCat member libraries worldwide
2 editions published in 1987 in English and held by 66 WorldCat member libraries worldwide
An multigrid LUSSOR scheme for approximate Newton iteration applied to the Euler equations
by
Seokkwan Yoon(
Book
)
1 edition published in 1986 in English and held by 65 WorldCat member libraries worldwide
1 edition published in 1986 in English and held by 65 WorldCat member libraries worldwide
A comparative study of the nonuniqueness problem of the potential equation
by
M. D Salas(
Book
)
1 edition published in 1985 in English and held by 54 WorldCat member libraries worldwide
1 edition published in 1985 in English and held by 54 WorldCat member libraries worldwide
Computational mathematics driven by industrial problems : lectures given at the 1st session of the Centro internazionale matematico estivo (C.I.M.E.) held in Martina Franca, Italy, June 2127, 1999
by
Rainer E Burkard(
)
3 editions published in 2000 in English and held by 24 WorldCat member libraries worldwide
These lecture notes by very authoritative scientists survey recent advances of mathematics driven by industrial application showing not only how mathematics is applied to industry but also how mathematics has drawn benefit from interaction with realword problems. The famous David Report underlines that innovative high technology depends crucially for its development on innovation in mathematics. The speakers include three recent presidents of ECMI, one of ECCOMAS (in Europe) and the president of SIAM
3 editions published in 2000 in English and held by 24 WorldCat member libraries worldwide
These lecture notes by very authoritative scientists survey recent advances of mathematics driven by industrial application showing not only how mathematics is applied to industry but also how mathematics has drawn benefit from interaction with realword problems. The famous David Report underlines that innovative high technology depends crucially for its development on innovation in mathematics. The speakers include three recent presidents of ECMI, one of ECCOMAS (in Europe) and the president of SIAM
Analysis of wing slipstream flow interaction
by
Antony Jameson(
Book
)
3 editions published in 1970 in English and held by 16 WorldCat member libraries worldwide
3 editions published in 1970 in English and held by 16 WorldCat member libraries worldwide
Supercritical wing sections II : a handbook
by
Frances Bauer(
)
4 editions published in 1975 in English and Undetermined and held by 15 WorldCat member libraries worldwide
4 editions published in 1975 in English and Undetermined and held by 15 WorldCat member libraries worldwide
Essential elements of computational algorithms for aerodynamic analysis and design
by
Antony Jameson(
Book
)
4 editions published in 1997 in English and held by 7 WorldCat member libraries worldwide
Abstract: "This paper traces the development of computational fluid dynamics as a tool for aircraft design. It addresses the requirements for effective industrial use, and tradeoffs between modeling accuracy and computational costs. Essential elements of algorithm design are discussed in detail, together with a unified approach to the design of shock capturing schemes. Finally, the paper discusses the use of techniques drawn from control theory to determine optimal aerodynamic shapes. In the future multidisciplinary analysis and optimization should be combined to provide an integrated design environment."
4 editions published in 1997 in English and held by 7 WorldCat member libraries worldwide
Abstract: "This paper traces the development of computational fluid dynamics as a tool for aircraft design. It addresses the requirements for effective industrial use, and tradeoffs between modeling accuracy and computational costs. Essential elements of algorithm design are discussed in detail, together with a unified approach to the design of shock capturing schemes. Finally, the paper discusses the use of techniques drawn from control theory to determine optimal aerodynamic shapes. In the future multidisciplinary analysis and optimization should be combined to provide an integrated design environment."
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Related Identities
 Research Institute for Advanced Computer Science (U.S.)
 Langley Research Center
 Institute for Computer Applications in Science and Engineering
 United States National Aeronautics and Space Administration
 Reuther, James Author
 Hafez, M. M. Editor
 Caughey, D. A. (David A.)
 Yoon, Seokkwan Author
 Reuther, J. Author
 Martinelli, Luigi
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Associated Subjects
Aerodynamics Aerodynamics, SupersonicComputer programs Aerodynamics, TransonicMathematical models AerodynamicsMathematical models Aerofoils Aircraft drafting AirplanesControl systems AirplanesWings Approximation theory Boundary layer Computeraided design Computer algorithms Control theory Diffusion Distribution (Probability theory) Economics Elmer A. Sperry Award Euler's numbers Finite volume method Flight control Fluid dynamics Fluid dynamicsComputer programs Fluid dynamicsData processing Fluid dynamicsMathematical models Fluid mechanics Gas dynamics Group schemes (Mathematics) Iterative methods (Mathematics) Lagrange equations Mach number Mathematical models Mathematical optimization Mathematics MathematicsIndustrial applications Multigrid methods (Numerical analysis) NavierStokes equations NavierStokes equationsNumerical solutions Numerical analysis Numerical grid generation (Numerical analysis) Potential theory (Mathematics) Shock waves Thermodynamics Transportation engineeringAwards United States Wings (Anatomy)