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Showing 1 to 20 of 36 for “"aerodynamic design"”.

  1. Aerodynamic design of annular ducts

    … presents mathematical and numerical methods for designing axisymmetric annular ducts having geometries capable of supporting fluid flows with prescribed performance characteristics. Three basic numerical methods of solution are given and are used to obtain results to the known exact solutions for …

    london-metro Repository record for Aerodynamic design of annular ducts (opens in a new tab)

  2. Hybrid Methods for Inverse Aerodynamic Design

    … to the development of inverse methods for the design of (1) multi-element airfoils for multipoint velocity and boundary-layer prescriptions and (2) airfoils to obtain desired multipoint velocity distributions on three-dimensional wings and complex juncture regions. These methods are discussed …

    uiuc Repository record for Hybrid Methods for Inverse Aerodynamic Design (opens in a new tab)

  3. Aerodynamic design optimization using flow feature parameterization

    Design optimization methods using high-fidelity computational fluid dynamics simulations are becoming increasingly popular in the area of aerodynamic design, sustaining the desire to make these methods more computationally efficient. Such design strategies typically define the aerodynamic product …

    soton Repository record for Aerodynamic design optimization using flow feature parameterization (opens in a new tab)

  4. Aerodynamic design of an aspirated counter-rotating compressor

    A primary goal in compressor design for jet engines is the reduction of size and weight. This can be achieved by increasing the work output per stage, thereby reducing the required number of stages. In this thesis, the aerodynamic design of a high speed compressor that produces a pressure ratio of …

    mit Repository record for Aerodynamic design of an aspirated counter-rotating compressor (opens in a new tab)

  5. Gradient-Based Optimum Aerodynamic Design Using Adjoint Methods

    … are applied to a pressure-matching inverse design problem of quasi 1-D nozzle flows. Pontryagin’s Minimum Principle is used to derive the adjoint system and the reduced gradient of the cost functional. The properties of adjoint variables at the sonic throat and the shock location are …

    vt Repository record for Gradient-Based Optimum Aerodynamic Design Using Adjoint Methods (opens in a new tab)

  6. Optimization Techniques Exploiting Problem Structure: Applications to Aerodynamic Design

    … the use of all-at-once methods applied to aerodynamic design. All-at-once schemes are usually based on the assumption of sufficient continuity in the constraints and objectives, and this assumption can be troublesome in the presence of shock discontinuities. Special treatment has to be …

    vt Repository record for Optimization Techniques Exploiting Problem Structure: Applications to Aerodynamic Design (opens in a new tab)

  7. Performance evaluation and improvements of CFD-based aerodynamic design optimization

    … flow solvers, optimization methods, and design variables on aerodynamic design optimization. The Euler, Euler/boundary-layer, and compressible and incompressible Navier-Stokes equations were used for the flow analyses. Inverse design optimization used a least-square method to minimize …

    uiuc Repository record for Performance evaluation and improvements of CFD-based aerodynamic design optimization (opens in a new tab)

  8. Aerodynamic design and analysis of small horizontal axis wind turbine blades

    … out to be essential. This work investigates the aerodynamic design and analysis of small horizontal axis wind turbine blades via the blade element momentum (BEM) based approach and the computational fluid dynamics (CFD) based approach. From this research, it is possible to draw a series of …

    cent-lancashire Repository record for Aerodynamic design and analysis of small horizontal axis wind turbine blades (opens in a new tab)

  9. Two-dimensional transonic aerodynamic design and analysis using the Euler equations

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1986.

    mit Repository record for Two-dimensional transonic aerodynamic design and analysis using the Euler equations (opens in a new tab)

  10. Facilitating the Use of Optimisation in the Aerodynamic Design of Axial Compressors

    There is commercial pressure to design axial compressors exhibiting high levels of performance more quickly. This is despite the performance of these machines approaching an asymptote in recent years, with further gains becoming increasingly difficult to achieve. One tool that can be used to help …

    cambridge Repository record for Facilitating the Use of Optimisation in the Aerodynamic Design of Axial Compressors (opens in a new tab)

  11. Control and Aerodynamic Design of a Solar Road Vehicle with Articulated Surfaces

    … change. However, solar road vehicles—though designed and fabricated by some—have not reached a sufficient level to be production-worthy. The low efficiency of solar cells and the high energy demands of the average land vehicle are irreconcilable for most manufacturers using industry methods …

    mit Repository record for Control and Aerodynamic Design of a Solar Road Vehicle with Articulated Surfaces (opens in a new tab)

  12. Aerodynamic design of moveable inlet guide vanes for active control of rotating stall

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990.

    mit Repository record for Aerodynamic design of moveable inlet guide vanes for active control of rotating stall (opens in a new tab)

  13. An Analytical Asymptotic Solution Method of the Euler Equations for Efficient Flow Analysis and Aerodynamic Design

    An efficient flow analysis and aerodynamic design tool was developed based on analytical asymptotic solutions of the Euler equations. The solution algorithm uses an analytical asymptotic formulation in the streamline coordinate system, wherein the governing equations are transformed into a …

    uiuc Repository record for An Analytical Asymptotic Solution Method of the Euler Equations for Efficient Flow Analysis and Aerodynamic Design (opens in a new tab)

  14. A second generation URANS approach for application to aerodynamic design and optimization in the automotive industry

    … source of carbon emissions and air pollution. Aerodynamics is an important aspect for energy saving and emission reduction in the automotive industry. In the design stage, aerodynamic drag is minimized through optimization of the vehicle shape, and Computational Fluid Dynamics (CFD) has become …

    mit Repository record for A second generation URANS approach for application to aerodynamic design and optimization in the automotive industry (opens in a new tab)

  15. Aerodynamic Design Sensitivities on an Unstructured Mesh Using the Navier-Stokes Equations and a Discrete Adjoint Formulation

    … adjoint method is developed and demonstrated for aerodynamic design optimization on unstructured grids. The governing equations are the three-dimensional Reynolds-averaged Navier-Stokes equations coupled with a one-equation turbulence model. A discussion of the numerical implementation of the flow …

    vt Repository record for Aerodynamic Design Sensitivities on an Unstructured Mesh Using the Navier-Stokes Equations and a Discrete Adjoint Formulation (opens in a new tab)

  16. Development of S3D and Adjoint Design Methods for Efficient Aerodynamic Design of Three-Dimensional High-Speed Compressor Blades

    In the second part of the study, an adjoint design method was employed for compressor design to broaden the range of design capability, to facilitate 3D design applications, and to complement the S3D design method. An adjoint design code was developed, based on a 3D compressor flow analysis code, …

    uiuc Repository record for Development of S3D and Adjoint Design Methods for Efficient Aerodynamic Design of Three-Dimensional High-Speed Compressor Blades (opens in a new tab)

  17. A Computer Program for the Coupled Implementation of Meanline and Throughflow Methods to Simplify the Aerodynamic Design of Multistage Axial Compressors

    … program capable of simplifying the preliminary aerodynamic design process of multistage axial compressors has been developed. This interactive design tool, named C-STAAC, combines the Meanline and Throughflow analysis capabilities of two independent compressor design codes to form one standalone …

    embry-riddle Repository record for A Computer Program for the Coupled Implementation of Meanline and Throughflow Methods to Simplify the Aerodynamic Design of Multistage Axial Compressors (opens in a new tab)

  18. The design of adaptive structures for wing morphing

    This research is concerned with the design of adaptive structures for achieving global multi-shape morphing aerodynamic configurations, by using slender structures. The proposed methodologies pursue two threads towards global optimisation of morphing structures, by providing means of aerodynamic

    soton Repository record for The design of adaptive structures for wing morphing (opens in a new tab)

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