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Effect of local pressure transients on the deformations and stresses in cylindrical ducts. Volume I - Theory and design chartsAxially symmetric dynamic response solutions for cylinders subjected to pressure transients arising in propulsion systems
Document ID
19660026674
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Padlog, J. (Bell Aerosystems Co. Buffalo, NY, United States)
Reismann, H. (Bell Aerosystems Co. Buffalo, NY, United States)
Date Acquired
August 3, 2013
Publication Date
June 26, 1966
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-77774
Report Number: NASA-CR-77774
Accession Number
66N35964
Funding Number(s)
CONTRACT_GRANT: NAS8-11215
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PROPULSION SYSTEM
CYLINDER
AXISYMMETRIC DEFORMATION
TRANSIENT PRESSURE
DYNAMIC RESPONSE

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