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Transonic aerodynamic design experienceAdvancements have occurred in transonic numerical simulation that place aerodynamic performance design into a relatively well developed status. Efficient broad band operating characteristics can be reliably developed at the conceptual design level. Recent aeroelastic and separated flow simulation results indicate that systematic consideration of an increased range of design problems appears promising. This emerging capability addresses static and dynamic structural/aerodynamic coupling and nonlinearities associated with viscous dominated flows.
Document ID
19890011563
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bonner, E.
(Rockwell International Corp. Los Angeles, CA, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1989
Publication Information
Publication: NASA, Langley Research Center, Transonic Symposium: Theory, Application, and Experiment, Volume 1, Part 1
Subject Category
Aerodynamics
Accession Number
89N20934
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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