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Aerolastic tailoring and integrated wing designMuch has been learned from the TSO optimization code over the years in determining aeroelastic tailoring's place in the integrated design process. Indeed, it has become apparent that aeroelastic tailoring is and should be deeply embedded in design. Aeroelastic tailoring can have tremendous effects on the design loads, and design loads affect every aspect of the design process. While optimization enables the evaluation of design sensitivities, valid computational simulations are required to make these sensitivities valid. Aircraft maneuvers simulated must adequately cover the plane's intended flight envelope, realistic design criteria must be included, and models among the various disciplines must be calibrated among themselves and with any hard-core (e.g., wind tunnel) data available. The information gained and benefits derived from aeroelastic tailoring provide a focal point for the various disciplines to become involved and communicate with one another to reach the best design possible.
Document ID
19890015796
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Love, Mike H.
(General Dynamics Corp. Fort Worth, TX, United States)
Bohlmann, Jon
(General Dynamics Corp. Fort Worth, TX, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1989
Publication Information
Publication: NASA. Langley Research Center, Recent Advances in Multidisciplinary Analysis and Optimization, Part 1
Subject Category
Aircraft Design, Testing And Performance
Accession Number
89N25167
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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