Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity:
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Title
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity:
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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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AF TR 5761 Part 13
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Index Price
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$0.00
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Report Availability
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Not available via Contrails
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Creator
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Sechler, E. E.
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Dixon, H. H.
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Date
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1950
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Date Issued
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1950-12-01
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Extent
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235
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Corporate Author
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Guggenheim Aeronautical Laboratory
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Laboratory
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Air Materiel Command
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Identifier
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AD0108562
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Contract
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W33-038-ac-16961
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Distribution Classification
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2
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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