국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Advanced Usage of Vehicle Sketch Pad for CFD-Based Conceptual Design
저자	Ordaz, Irian;; Li, Wu
Keyword	AIRCRAFT DESIGN;; COMPUTATIONAL FLUID DYNAMICS;; COMPUTERIZED SIMULATION;; DESIGN ANALYSIS;; DESIGN OPTIMIZATION;; FINITE ELEMENT METHOD;; SHAPES
URL	http://hdl.handle.net/2060/20130003231
보고서번호	AIAA Paper 2013-0329
발행년도	2013
출처	NTRS (NASA Technical Report Server)
ABSTRACT	Conceptual design is the most fluid phase of aircraft design. It is important to be able to perform large scale design space exploration of candidate concepts that can achieve the design intent to avoid more costly configuration changes in later stages of design. This also means that conceptual design is highly dependent on the disciplinary analysis tools to capture the underlying physics accurately. The required level of analysis fidelity can vary greatly depending on the application. Vehicle Sketch Pad (VSP) allows the designer to easily construct aircraft concepts and make changes as the design matures. More recent development efforts have enabled VSP to bridge the gap to high-fidelity analysis disciplines such as computational fluid dynamics and structural modeling for finite element analysis. This paper focuses on the current state-of-the-art geometry modeling for the automated process of analysis and design of low-boom supersonic concepts using VSP and several capability-enhancing design tools.