The contents of this report are presented to emphasize a possible approach to establishing useable design philosophies for utilizing Fiber Reinforced Composites for major airframe components. It outlines the general nature of these materials with accompanying thoughts for assessing the material characteristics. Advantages and disadvantages of these materials are listed, with more emphasis on areas of needed research. An attempt is made to associate these research areas with the appropriate technical field of interest.
Philosophy for the Design of Primary Aircraft Structures with Fibrous Reinforced Composites (Frc)
1964
2 pages
Report
No indication
English
AIRFRAMES , COMPOSITE MATERIALS , REINFORCING MATERIALS , FIBERS , GLASS TEXTILES , PLASTICS , LAMINATED PLASTICS , FATIGUE (MECHANICS) , FAILURE (MECHANICS) , FILAMENT WOUND CONSTRUCTION , SANDWICH PANELS , HONEYCOMB CORES , STRUCTURAL PROPERTIES , AERODYNAMIC CHARACTERISTICS , LOADING (MECHANICS) , AIRFOILS
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