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Economic evaluation of flying-qualities design criteria for a transport configured with relaxed static stabilityDirect constrained parameter optimization was used to optimally size a medium range transport for minimum direct operating cost. Several stability and control constraints were varied to study the sensitivity of the configuration to specifying the unaugmented flying qualities of transports designed to take maximum advantage of relaxed static stability augmentation systems. Additionally, a number of handling qualities related design constants were studied with respect to their impact on the design.
Document ID
19810005457
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Sliwa, S. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1980
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TP-1760
L-13944
Accession Number
81N13968
Funding Number(s)
PROJECT: RTOP 505-34-33-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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