dc.contributor.advisor |
Morris, Alan J. |
|
dc.contributor.author |
Alsina, J. |
|
dc.date.accessioned |
2009-06-10T15:24:52Z |
|
dc.date.available |
2009-06-10T15:24:52Z |
|
dc.date.issued |
1988-04 |
|
dc.identifier.uri |
http://hdl.handle.net/1826/3442 |
|
dc.description.abstract |
The aircraft design process is characterised by the application
of a wide range of knowledge across many disciplines based upon a
certain degree of judgement and experience of the designer. A two
pass approach has been taken towards the development of an aircraft
design expert system based on the requirements of two conceptually
different design steps namely, wing design and aircraft configuration.
The current status of the work is one where an actual program for wing
design exists with supporting documentation, and a very effective
examination of the knowledge base performed based on the detail
investigation of overall aircraft design process with particular
emphasis on the wing design and the aircraft configuration design
steps.
The approach taken accomplishes the objectives of the current
research in defining the knowledge base, providing tools and
specifications for tools to be used within an aircraft design expert
system closely following the problem-solving techniques utilised by
the design expert. |
en_UK |
dc.language.iso |
en |
en_UK |
dc.publisher |
Cranfield University |
en_UK |
dc.title |
Development of an aircraft design expert system |
en_UK |
dc.type |
Thesis or dissertation |
en_UK |
dc.type.qualificationlevel |
Doctoral |
en_UK |
dc.type.qualificationname |
PhD |
en_UK |