Title:
Integrated Product Development for the Wing Structural Design of the High Speed Civil Transport

dc.contributor.author Marx, William J. en_US
dc.contributor.author Mavris, Dimitri N. en_US
dc.contributor.author Schrage, Daniel P. en_US
dc.contributor.corporatename American Institute of Aeronautics and Astronautics
dc.contributor.corporatename Georgia Institute of Technology. Aerospace Systems Design Laboratory
dc.date.accessioned 2005-05-26T14:02:45Z
dc.date.available 2005-05-26T14:02:45Z
dc.date.issued 1994-09 en_US
dc.description Presented at the 5th AIAA/NASA/USAF/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Panama City, FL, September 7-9, 1994. en_US
dc.description.abstract The extent of knowledge required to perform the task of integrating manufacturing with aircraft design is beyond the expertise of a single engineer. This defines the need for a decision support system, or Knowledge-Based System, to aid the engineer in performing parallel product and process trades. This paper describes a research effort that includes development and integration of a manufacturing knowledge base and a rule-based reasoning system. NASA interests in the research discussed in this paper are directly related to their High Speed Research program. According to the program, NASA and this country's aerospace industry have undertaken the challenge of designing and building a 2 nd generation supersonic commercial transport by the early 21 st century. The proposed aircraft, called the High Speed Civil Transport, is envisioned to cruise at Mach 2.4 and carry 300 passengers to destinations in excess of 5,000 nautical miles. In addition, this aircraft must be economically viable and affordable, while being environmentally friendly and abiding by all appropriate FAR and EPA requirements. Integrated Product Development techniques aimed at assessing producibility can help designers perform the necessary trade-off studies to design the strongest, lightest possible structure at the least cost that meets the load-carrying requirement for a specified aircraft range. This concurrent design requires an integration of design with manufacturing and an optimization process that will consider design trade-offs related to product performance, producibility, and support. This integrated design and manufacturing approach can be used to develop low cost, producible structural design concepts. This approach involves encoding the knowledge of human experts concerning aircraft manufacturing and design into an appropriate representation. The seamless integration of a manufacturing Knowledge-Based System with aircraft preliminary design and analysis tools will yield a concurrent engineering system that will assist aerospace systems designers in performing parallel product and process design trades. en_US
dc.format.extent 75314 bytes
dc.format.mimetype application/pdf
dc.identifier.uri http://hdl.handle.net/1853/6347
dc.language.iso en_US en_US
dc.publisher Georgia Institute of Technology en_US
dc.publisher Georgia Institute of Technology
dc.publisher.original American Institute of Aeronautics and Astronautics (AIAA)
dc.relation.ispartofseries ASDL;AIAA-94-4253 en_US
dc.relation.ispartofseries ASDL;AIAA-94-4253
dc.subject Integrated product and process development en_US
dc.subject Wings en_US
dc.subject Structural design en_US
dc.subject High-Speed Civil Transport en_US
dc.subject Decision-making en_US
dc.subject Optimization en_US
dc.subject Aerospace systems en_US
dc.title Integrated Product Development for the Wing Structural Design of the High Speed Civil Transport en_US
dc.type Text
dc.type.genre Paper
dspace.entity.type Publication
local.contributor.author Mavris, Dimitri N.
local.contributor.corporatename Daniel Guggenheim School of Aerospace Engineering
local.contributor.corporatename Aerospace Systems Design Laboratory (ASDL)
local.contributor.corporatename College of Engineering
relation.isAuthorOfPublication d355c865-c3df-4bfe-8328-24541ea04f62
relation.isOrgUnitOfPublication a348b767-ea7e-4789-af1f-1f1d5925fb65
relation.isOrgUnitOfPublication a8736075-ffb0-4c28-aa40-2160181ead8c
relation.isOrgUnitOfPublication 7c022d60-21d5-497c-b552-95e489a06569
Files
Original bundle
Now showing 1 - 1 of 1
Thumbnail Image
Name:
AIAA-94-4253.pdf
Size:
73.55 KB
Format:
Adobe Portable Document Format
Description: