Measurement of Angular Displacements of Practical Wing Structures by the Moire' Fringe Technique
Item
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Title
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Measurement of Angular Displacements of Practical Wing Structures by the Moire' Fringe Technique
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Date
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1964
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Index Abstract
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Coming Soon
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Photo Quality
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Complete
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Report Number
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FDL TDR 64-42
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Creator
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Padlog, Joseph
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Gallagher, Richard H.
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Corporate Author
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Bell Aerosystems Company
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Laboratory
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AF Flight Dynamics Laboratory
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Extent
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56
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Identifier
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AD0608470
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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(657)-7486
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DoD Project
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8219
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DoD Task
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821901
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DTIC Record Exists
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No
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Distribution Change Authority Correspondence
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None
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Abstract
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Results of a study of the feasibility of employing the Moire' fringe technique in the measurement of angular displacements of practical wing structures are presented. Slope influence coefficients obtained from Moire' fringe patterns determined from a square cantilever plate and a swept wing model are compared with available theoretical and experimental data.
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Report Availability
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Full text available
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Date Issued
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1964-09
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Provenance
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Lockheed Martin Missiles & Fire Control
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Type
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report
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Format
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1 online resource