Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722053635
Category :
Languages : en
Pages : 38
Book Description
A scheme is developed for solving constrained optimization problems in which the objective function and the constraint function are dependent on the solution of the nonlinear flow equations. The scheme updates the design parameter iterative solutions and the flow variable iterative solutions simultaneously. It is applied to an advanced propeller design problem with the Euler equations used as the flow governing equations. The scheme's accuracy, efficiency and sensitivity to the computational parameters are tested. Rizk, Magdi H. Unspecified Center NAS3-24855; SBIR-01.01-8500; RTOP 535-03-01...
Aerodynamic Optimization by Simultaneously Updating Flow Variables and Design Parameters with Application to Advanced Propeller Designs
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722053635
Category :
Languages : en
Pages : 38
Book Description
A scheme is developed for solving constrained optimization problems in which the objective function and the constraint function are dependent on the solution of the nonlinear flow equations. The scheme updates the design parameter iterative solutions and the flow variable iterative solutions simultaneously. It is applied to an advanced propeller design problem with the Euler equations used as the flow governing equations. The scheme's accuracy, efficiency and sensitivity to the computational parameters are tested. Rizk, Magdi H. Unspecified Center NAS3-24855; SBIR-01.01-8500; RTOP 535-03-01...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722053635
Category :
Languages : en
Pages : 38
Book Description
A scheme is developed for solving constrained optimization problems in which the objective function and the constraint function are dependent on the solution of the nonlinear flow equations. The scheme updates the design parameter iterative solutions and the flow variable iterative solutions simultaneously. It is applied to an advanced propeller design problem with the Euler equations used as the flow governing equations. The scheme's accuracy, efficiency and sensitivity to the computational parameters are tested. Rizk, Magdi H. Unspecified Center NAS3-24855; SBIR-01.01-8500; RTOP 535-03-01...
Scientific and Technical Aerospace Reports
Special Course on Inverse Methods for Airfoil Design for Aeronautical and Turbomachinery Applications
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 564
Book Description
"This lecture series is devoted to major aspects of aerofoil design both for aeronautical and turbomachine application. These include: (1) optimisation of target pressure and velocity distribution. Both direct optimisation resulting from an inverse boundary layer calculation and an iterative optimisation of the loses are presented. (2) aerofoil design by means of inverse methods. This ranges from simple parametric definitions of two- dimensional cross sections to a detailed numerical definition of three dimensional shapes. blade or airfoil designs are normally made in two steps, and the lectures are accordingly grouped into two parts. First, optimisation of target pressure and velocity distributions are discussed taking into account the required performance and the lost mechanisms in the boundary layer. Both direct optimisation resulting from an inverse boundary layer calculation, and an iterative optimisation by minimisation of the losses are presented. It is clear from both procedures that inclusion of off-design operation is one of the greatest difficulties involved in blade or airfoil operation. The second part gives an overview of the numerous inverse blade design methods that have been developed both for turbomachinery and aeronautical applications. This ranges from simple parameter definitions of two-dimensional cross-sections to the full three-dimensional definition of wings and blade channels."--DTIC.
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 564
Book Description
"This lecture series is devoted to major aspects of aerofoil design both for aeronautical and turbomachine application. These include: (1) optimisation of target pressure and velocity distribution. Both direct optimisation resulting from an inverse boundary layer calculation and an iterative optimisation of the loses are presented. (2) aerofoil design by means of inverse methods. This ranges from simple parametric definitions of two- dimensional cross sections to a detailed numerical definition of three dimensional shapes. blade or airfoil designs are normally made in two steps, and the lectures are accordingly grouped into two parts. First, optimisation of target pressure and velocity distributions are discussed taking into account the required performance and the lost mechanisms in the boundary layer. Both direct optimisation resulting from an inverse boundary layer calculation, and an iterative optimisation by minimisation of the losses are presented. It is clear from both procedures that inclusion of off-design operation is one of the greatest difficulties involved in blade or airfoil operation. The second part gives an overview of the numerous inverse blade design methods that have been developed both for turbomachinery and aeronautical applications. This ranges from simple parameter definitions of two-dimensional cross-sections to the full three-dimensional definition of wings and blade channels."--DTIC.
Aeronautical Engineering
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1040
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1040
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1038
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1038
Book Description
Multidisciplinary Applications of Computational Fluid Dynamics
Author: American Society of Mechanical Engineers. Winter Annual Meeting
Publisher: American Society of Mechanical Engineers
ISBN:
Category : Mathematics
Languages : en
Pages : 128
Book Description
Publisher: American Society of Mechanical Engineers
ISBN:
Category : Mathematics
Languages : en
Pages : 128
Book Description