Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure: Supplement I - Dynamic Modeling of Complex Structures
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: Supplement I - Dynamic Modeling of Complex Structures
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Index Abstract
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Not Available
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Photo Quality
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Incomplete
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Report Number
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ASD TDR 62-801 Supplement I
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Index Price
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$0.00
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Report Availability
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Full text available by request
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Creator
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Roberts, W. H.
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Finwall, P. E.
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Date
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1964
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Extent
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249
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Laboratory
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AF Flight Dynamics Laboratory
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Identifier
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AD0600234
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Corporate Report Number
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NOR 63-139
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Contract
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AF 33(657)-10075
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DoD Project
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1370
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DoD Task
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137005
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Distribution Conflict
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No
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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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Special Scanning Requirements
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Foldout pages
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Date Issued
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1964-04
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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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Bombardier/Aero
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Type
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report