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Bonded Aircraft Structures for General Aviation
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Language:
English
Abstract
Adhesive bonding offers structural efficiency, lower weight, reduced production costs and improved appearance to the general aviation industry. To achieve these advantages, the design and production techniques must be geared to the product operational environment and cost limitation of the general aviation industry.
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Authors
Topic
Citation
Steiner, N., "Bonded Aircraft Structures for General Aviation," SAE Technical Paper 700221, 1970, https://doi.org/10.4271/700221.Also In
References
- Pazymany L. “Potential Structural Materials and Design Concepts for Light Airplanes” October 1968
- “Bonded Aircraft Structures.” Bonded Structures Limited Duxford, Cambridge, England
- “Bonded Aircraft Structures.” Cambridge Aero Research Limited Duxford, Cambridge, England 1957
- Federal Adhesive Specification MMM-A-132 “Adhesives, Heat Resistant, Airframe Structural, Metal-To-Metal.”
- Cagle C. V. “Adhesive Bonding.” N. Y. McGraw-Hill 1968
- “Metlbond 225 Adhesive.” Product information data Whittaker Corp., Narmco Materials Div. Costa Mesa, Cal 1966
- “Durability of Adhesive Joints.” ASTM
- “Determination of Mechanical Properties of Adhesives for Use in the Design of Bonded Joints.” USDA Forest Products Laboratory Madison, Wis.
- Greenwood D. “Product Engineering Design Manual.” McGraw-Hill
- Snogren R. C. “Bonding Materials-Adhesive Bonding Metals.” ASME May 1969
- deBruyne Houwink “Adhesion and Adhesives.” New York 1951