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Mach 3 Wing Structures Stiffened Skin versus Sandwich
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English
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Joanides, J., Mellin, S., and Lackman, L., "Mach 3 Wing Structures Stiffened Skin versus Sandwich," SAE Technical Paper 610016, 1961, https://doi.org/10.4271/610016.Also In
References
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- Seydel Edgar Wrinkling of Reinforced Plates Subjected to Shear Stresses NACA, TM 602 January 1931
- Sandwich Construction for Aircraft Part II, MIL-HDBK-23
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- Timoshenko S. Theory of Plates and Shells McGraw-Hill Publishing Co., Inc. 1940
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- Wittrick W. H. Correlation Between Some Stability Problems for Orthotropic and Isotropic Plates Under BI-Axial and UNI-Axial Direct Stress The Aeronautical Quarterly August 1952