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Computational, unsteady transonic aerodynamics and aeroelasticity about airfoils and wings

Author
Goorjian, Peter M.
Published
Jan 1, 1987.
Physical Description
1 electronic document
Additional Creators
Guruswamy, Guru P.
Online Version

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Research in the area of computational, unsteady transonic flows about airfoils and wings, including aeroelastic effects is reviewed. In the last decade, there have been extensive developments in computational methods in response to the need for computer codes with which to study fundamental aerodynamic and aeroelastic problems in the critical transonic regime. For example, large commercial aircraft cruise most effectively in the transonic flight regime and computational fluid dynamics (CDF) provides a new tool, which can be used in combination with test facilities to reduce the costs, time, and risks of aircraft development.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19870007368.
Accession ID: 87N16801.
A-87042.
NAS 1.15:89414.
NASA-TM-89414.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15700679