Data on the Compressive Strength of Skin-stringer Panels of Various Materials
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MAGNESIUM↗
Engineering topics
Hickman, William A
Publications and source records attributed to Hickman, William A.
Effect of variation in rivet strength on the average stress at maximum load for aluminum-alloy, flat, z-stiffened compression panels that fail by local buckling
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Dow, Norris F↗
Direct-reading Design Charts for 24S-T3 Aluminum-alloy Flat Compression Panels Having Longitudinal Formed Hat-section Stiffeners and Comparisons with Panels Having Z-section Stiffeners
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Hickman, William A↗
Preliminary Experiments on the Elastic Compressive Buckling of Plates with Integral Waffle-like Stiffening
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Dow, Norris F↗
Direct-reading design charts for 75S-T6 aluminum-alloy flat compression panels having longitudinal extruded Z-section stiffeners
Direct-reading design charts are presented for 75S-T6 aluminum-alloy flat compression panels having longitudinal extruded Z-section stiffeners. These charts, which cover a wide range of proportions, make possible the direct determination of the stress and all panel dimensions required to carry a given intensity of loading with a given skin thickness and effective length of panel.
Hickman, William A↗
Effect of variation in rivet diameter and pitch on the average stress at maximum load for 24S-T3 and 75S-T6 aluminum-alloy, flat, Z-stiffened panels that fail by local instability
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ALUMINUM ALLOYS - ALCOA 75ST6↗
Data on the Compressive Strength of 75S-T6 Aluminum-Alloy Flat Panels Having Small, Thin, Widely Spaced, Longitudinal Extruded Z-Section Stiffeners
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ALUMINUM ALLOYS - EXTRUSION↗
Data on the Compressive Strength of 75S-T6 Aluminum-Alloy Flat Panels with Longitudinal Extruded Z-Section Stiffeners
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ALUMINUM ALLOYS - ALCOA 75ST6 - STRENGTH, COMPRESS↗
Comparison of the Structural Efficiency of Panels Having Straight-web and Curved-web Y-section Stiffeners
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STRESSED SKIN - PLATES↗
Effect of Variation in Diameter and Pitch of Rivets on Compressive Strength of Panels with Z-section Stiffeners : Panels that Fail by Local Buckling and Have Various Values of Width-to-thickness Ratio for the Webs of the Stiffeners
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RIVETS - SPACING↗
Direct-reading Design Charts for 75S-T Aluminum-alloy Flat Compression Panels Having Longitudinal Straight-web Y-section Stiffeners
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ALUMINUM ALLOYS, SHEET - ALCLAD 75ST - STRENGTH, C↗
Compressive Strength of 24S-T Aluminum-alloy Flat Panels with Longitudinal Formed Hat-section Stiffeners Having Four Ratios of Stiffener Thickness to Skin Thickness
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CHARTS - STRESSED SKIN↗
Structural Evaluation of an Extruded Magnesium-alloy T-stiffened Panel
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STRESSED SKIN-STIFFENER COMBINATIONS↗
Effect of Variation in Diameter and Pitch of Rivets on Compressive Strength of Panels with Z-section Stiffeners: Panels of Various Stiffener Spacings that Fail by Local Buckling
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STRESSED SKIN-STIFFENER COMBINATIONS - STRENGTH, C↗
Compressive Strength of 24S-T Aluminum-alloy Flat Panels with Longitudinal Formed Hat-section Stiffeners Having a Ratio of Stiffener Thickness to Skin Thickness Equal to 1.00
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STRESSED SKIN-STIFFENER COMBINATIONS - STRENGTH, C↗
Effect of Variation in Diameter and Pitch of Rivets on Compressive Strength of Panels with Z-section Stiffeners : Panels of Various Lengths with Close Stiffener Spacing
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STRESSED SKIN-STIFFENER COMBINATIONS - STRENGTH, C↗
Design Charts for Flat Compression Panels Having Longitudinal Extruded Y-section Stiffeners and Comparison with Panels Having Formed Z-section Stiffeners
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ALUMINUM ALLOYS, SHEET - ALCLAD 75ST - STRENGTH, C↗
Compressive-strength Comparisons of Panels Having Aluminum-alloy Sheet and Stiffeners with Panels Having Magnesium-alloy Sheet and Aluminum Alloy Stiffeners
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STRESSED SKIN - WINGS↗