Study on Project Design Process of Aircraft

Yong Feng Shang

doi:10.4028/www.scientific.net/AMM.353-356.3695

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 353-356Study on Project Design Process of Aircraft

Study on Project Design Process of Aircraft

Abstract:

The integration of the aircraft design process requires careful management of the computer information system to avoid the use of different standards yet to allow changes to be incorporated as the design develops. The aircraft project manager has to control the total system design. This requires different knowledge and skills to that of the traditional chief designer. Several different software suites have been developed to meet the requirements of 'computer-aided design'. Each of the major manufacturing companies has incorporated a specific CAD system which it standardizes for use in all the sections of the company; and they require subcontractors to be able to use a similar system.

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Periodical:

Applied Mechanics and Materials (Volumes 353-356)

Pages:

3695-3698

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.353-356.3695

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Online since:

August 2013

Authors:

Yong Feng Shang

Keywords:

Aircraft, Conceptual, Design, Preliminary Design, Project

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References

[1] Bolebaum, C.L. Formal and Heuristic System Decomposition in Structural Optimization [R]. NASA-CR-4413, (1991).

Google Scholar

[2] Raymer, D.P. Aircraft Design: A Conceptual Approach (M]. Washington D.C.: American Institute of Aeronautics and Astronautics, Inc., (1989).

Google Scholar

[3] Sobieszczanski-Sobieski, J. A Linear Decomposition Method for Large Optimization Problems一Blueprint for Development [R]. NASA TM-83248, (1982).

Google Scholar

[4] Sobieszczanski-Sobieski, J., Haftka, R.T. Multidisciplinary Aerospace Design Optimization: Survey of Recent Developments [C]. AIAA 96-0711.

DOI: 10.2514/6.1996-711

Google Scholar

[5] Barthelemy, J. -F., Wrenn, Cx and Dovi, A., et al. Integrating Aerodynamics and Structures in the Minimum Weight Design of a Supersonic Transport Wing [C]. AIAA 92-2372.

DOI: 10.2514/3.46491

Google Scholar

[6] Unger, E.R., Hutchison, M. Cz and Rais-Rohani, M., et al. Variable-Complexity Multidisciplinary Design of a Transport Wing [J]. International Journal of System Automation: Research and Applications (SARA), 1992, 2(2): 87-113.

Google Scholar