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Hypersonic flutter analysis using measured static aerodynamic derivatives, and comparison with experimentMeasured static aerodynamic forces for hypersonic flutter analysis on airfoil models in helium flow
Document ID
19690016893
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Goetz, R. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-5233
Report Number: NASA-TN-D-5233
Accession Number
69N26271
Funding Number(s)
CONTRACT_GRANT: 126-14-02-08-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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