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The flutter of towed rigid deceleratorsFlutter of towed rigid decelerators, and relationships between geometric and aerodynamic parameters defining unconditional stability boundary
Document ID
19670015723
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mac Neal, R. H. (Astro Research Corp. Santa Barbara, CA, United States)
Date Acquired
August 3, 2013
Publication Date
May 1, 1967
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-766
Report Number: NASA-CR-766
Accession Number
67N25052
Funding Number(s)
CONTRACT_GRANT: NAS1-5605
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TOWED BODY
STABILITY
DECELERATOR
FLUTTER

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