Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure
Item
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Title
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Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure
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Date
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1963
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Index Abstract
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Not Available
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Photo Quality
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Undetermined
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Report Number
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ASD TDR 62-801
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Creator
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Roberts, W. H.
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Finwall, P. E.
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White, R. W.
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Eldred, K. E.
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Corporate Author
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Northup Corporation
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Laboratory
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Flight Dynamics Laboratory
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Extent
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337
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Identifier
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AD0600234
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Access Rights
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OTS
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Distribution Classification
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1
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Contract
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AF 33(616)-8219
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DoD Project
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1370
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DoD Task
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137009
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DTIC Record Exists
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Yes
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Distribution Change Authority Correspondence
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None
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Distribution Conflict
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No
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Report Availability
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Full text available
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Date Issued
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1963-08
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Abstract
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The abstract for this report is either unavailable or has yet to be entered
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Provenance
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Jim Kinney
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Type
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report
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Format
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1 online resource