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Subsonic Wing Optimization for Handling Qualities Using ACSYNTThe capability to accurately and rapidly predict aircraft stability derivatives using one comprehensive analysis tool has been created. The PREDAVOR tool has the following capabilities: rapid estimation of stability derivatives using a vortex lattice method, calculation of a longitudinal handling qualities metric, and inherent methodology to optimize a given aircraft configuration for longitudinal handling qualities, including an intuitive graphical interface. The PREDAVOR tool may be applied to both subsonic and supersonic designs, as well as conventional and unconventional, symmetric and asymmetric configurations. The workstation-based tool uses as its model a three-dimensional model of the configuration generated using a computer aided design (CAD) package. The PREDAVOR tool was applied to a Lear Jet Model 23 and the North American XB-70 Valkyrie.
Document ID
19960054468
Acquisition Source
Ames Research Center
Document Type
Thesis/Dissertation
Authors
Soban, Danielle Suzanne
(California Polytechnic State Univ. San Luis Obispo, CA United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1996
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:202405
NASA-CR-202405
Report Number: NAS 1.26:202405
Report Number: NASA-CR-202405
Accession Number
96N36614
Funding Number(s)
CONTRACT_GRANT: NCC2-855
Distribution Limits
Public
Copyright
Public Use Permitted.
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