AIAA 2003–3429 High-Fidelity Aero-Structural Design Using a Parametric CAD-Based Model

نویسندگان

  • Juan J. Alonso
  • Joaquim R. R. A. Martins
  • James J. Reuther
چکیده

This paper presents two major additions to our high-fidelity aero-structural design environment. Our framework uses high-fidelity descriptions for both the flow around the aircraft (Euler and Navier-Stokes) and for the structural displacements and stresses (a full finite-element model) and relies on a coupled-adjoint sensitivity analysis procedure to enable the simultaneous design of the shape of the aircraft and its underlying structure to satisfy the measure of performance of interest. The first of these additions is a direct interface to a parametric CAD model that we call AEROSURF and that is based on the CAPRI Application Programming Interface (API). This CAD interface is meant to facilitate designs involving complex geometries where multiple surface intersections change as the design proceeds and are complicated to compute. In addition, the surface geometry information provided by this CAD-based parametric solid model is used as the common geometry description from which both the aerodynamic model and the structural representation are derived. The second portion of this work involves the use of the Finite Element Analysis Program (FEAP) for the structural analyses and optimizations. FEAP is a full-purpose finite element solver for structural models which has been adapted to work within our aero-structural framework. In addition, it is meant to represent the state-of-the-art in finite element modeling and it is used in this work to provide realistic aero-structural optimization costs for structural models of sizes typical in aircraft design applications. The capabilities of these two major additions are presented and discussed. The parametric CAD-based geometry engine, AEROSURF, is used in aerodynamic shape optimization and its performance is compared with our standard, in-house, geometry model. The FEAP structural model is used in optimizations using our previous version of AEROSURF (developed in-house) and is shown to provide realistic results with detailed structural models.

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

AIAA 2002–5402 Complete Configuration Aero-Structural Optimization Using a Coupled Sensitivity Analysis Method

This paper focuses on the demonstration of a new integrated aero-structural design method for aerospace vehicles. The approach combines an aero-structural analysis solver, a coupled aero-structural adjoint solver, a geometry-based analysis and design integration strategy, and an efficient gradient-based optimization algorithm. The aero-structural solver ensures highly accurate solutions by usin...

متن کامل

AIAA 2002–1483 High-Fidelity Aero-Structural Design Optimization of a Supersonic Business Jet

This paper focuses on the demonstration of an integrated aero-structural method for the design of aerospace vehicles. Both aerodynamics and structures are represented using high-fidelity models such as the Euler equations for the aerodynamics and a detailed finite element model for the primary structure. The aerodynamic outer mold line (OML) and a structure of fixed topology are parameterized u...

متن کامل

Unified Geometry Access for Analysis and Design

This paper presents a comprehensive approach for CAD based geometry handling in support of single and multidisciplinary analysis and design. Unlike previous schemes, the model presented here allows for hands-off automated meshing, a requirement for design studies. Multidisciplinary analysis is handled through solid modeling constructs, using the geometry as a transfer media. For design applicat...

متن کامل

A Coupled-Adjoint Sensitivity Analysis Method for High-Fidelity Aero-Structural Design

This paper presents an adjoint method for sensitivity analysis that is used in an aero-structural aircraft design framework. The aero-structural analysis uses high-fidelity models of both the aerodynamics and the structures. Aero-structural sensitivities are computed using a coupled-adjoint approach that is based on previously developed single discipline sensitivity analysis. Alternative strate...

متن کامل

pyMDO: A Framework for High-Fidelity Multi-Disciplinary Optimization

This paper presents a new approach to the software architecture of a high-fidelity multidisciplinary design framework that facilitates the reuse of existing components, the addition of new ones, and the scripting of MDO procedures. As a first step towards this goal, we implement the necessary components of a high-fidelity aero-structural design environment for complete aircraft configurations, ...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2003