Design of a canard configured TransCruiser using CEASIOM |
| |
| Authors: | Arthur Rizzi Peter Eliasson Tomasz Goetzendorf-Grabowski Jan B Vos Mengmeng Zhang Thomas S Richardson |
| |
| Institution: | aDepartment of Aeronautical and Vehicle Engineering, Royal Institute of Technology (KTH), Stockholm 10044, Sweden;bDepartment Aeronautics & Systems Technology, FOI, Swedish Defense Research Institute, 16490 Stockholm, Sweden;cInstitute of Aeronautics & Applied Mechanics, Aircraft Design Department, Warsaw University of Technology, 00-665 Warsaw, Poland;dCFS Engineering, PSE-A, 1015 Lausanne, Switzerland;eFaculty of Engineering, University of Bristol, University Walk, Bristol BS8 1TR, UK |
| |
| Abstract: | CEASIOM is a multidisciplinary software environment for aircraft design that has been developed as part of the European Framework 6 SimSAC project. It closely integrates discipline-specific tools such as those used for CAD, grid generation, CFD, stability analysis and control system design. The environment allows the user to take an initial design from geometry definition and aerodynamics generation through to full six degrees of freedom simulation and analysis. Key capabilities include variable fidelity aerodynamics tools and aeroelasticity modules. The purpose of this paper is to demonstrate the potential of CEASIOM by presenting the results of a Design, Simulate and Evaluate (DSE) exercise applied to a novel, project specific, transonic cruiser configuration called the TCR. The baseline TCR configuration is first defined using conventional methods, which is then refined and improved within the CEASIOM software environment. A wind tunnel model of this final configuration was then constructed, tested and used to verify the results generated using CEASIOM. |
| |
| Keywords: | Aircraft design Aerodynamics Flight dynamics Flight control CFD Simulation |
| 本文献已被 ScienceDirect 等数据库收录！ |
|
