NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Optimization of structures to satisfy aeroelastic requirementsA method for the optimization of structures to satisfy flutter velocity constraints is presented along with a method for determining the flutter velocity. A method for the optimization of structures to satisfy divergence velocity constraints is included.
Document ID
19750007567
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rudisill, C. S. (Clemson Univ. SC, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-142021
Report Number: NASA-CR-142021
Accession Number
75N15639
Funding Number(s)
CONTRACT_GRANT: NGR-41-001-027
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available