Books on the topic 'Epoxy Glass Fiber'

Keinanen, Heikki. Interlaminar mode-II fracture toughness of a glass-fiber epoxy laminate. Espoo, Finland: Technical Research Centre of Finland, 1992.

Aiken, David, and Zora Aiken. Fiberglass Repair: Polyester or Epoxy. Atglen: Cornell Maritime Press, 2008.

Mourad, Mouben. Fibre/matrix interaction in woven E-glass reinforced epoxy composites. Poole: Bournemouth University, 1995.

Xiong, June Yu. Visualization of the interphase failure in glass fibre reinforced epoxy composite. Ottawa: National Library of Canada, 1994.

Kensche, Christoph W. High cycle fatigue of glass fibre reinforced epoxy materials for wind turbines. Köln: Deutsche Forschungsanstalt für Luft- Und Raumfahrt, 1992.

Monitoring fiber stress during curing of single fiber glass- and graphite-epoxy composites. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

United States. National Aeronautics and Space Administration., ed. Ten year-environmental test of glass fiber/epoxy pressure vessels. [Washington, DC]: National Aeronautics and Space Administration, 1985.

Ten year-environmental test of glass fiber/epoxy pressure vessels. [Washington, DC]: National Aeronautics and Space Administration, 1985.

Ten year-environmental test of glass fiber/epoxy pressure vessels. [Washington, DC]: National Aeronautics and Space Administration, 1985.

P, Kosuri Ranga, Bowles Kenneth J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Monitoring fiber stress during curing of single fiber glass- and graphite-expoxy composites. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

C, Smith, Lumban-Tobing F, and Langley Research Center, eds. Analysis of thick sandwich shells with embedded ceramic tiles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

An examination of impact damage in glass/phenolic and aluminum honeycomb core composite panels. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

National Aeronautics and Space Administration and NASA. Composite Drill Stem of Epoxy Fiber Glass Reinforced with Boron Filaments and a Retrievable Core Liner/Sample Return Container for the Apollo Lunar Surface Drill: August 1 1970. Independently Published, 2022.

Aiken, David, and Zora Aiken. Fiberglass Repair: Polyester or Epoxy. Cornell Maritime Press, 2005.

Kevin, O'Brien T., Rousseau Carl Q, and United States. National Aeronautics and Space Administration., eds. Fatigue life methodology for tapered composite flexbeam laminates. [Washington, DC: National Aeronautics and Space Administration, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and United States. National Aeronautics and Space Administration., eds. Fatigue life methodology for tapered composite flexbeam laminates. [Washington, DC: National Aeronautics and Space Administration, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and Langley Research Center, eds. Fatigue life methodology for tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and Langley Research Center, eds. Fatigue life methodology for tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

S, Raju I., O'Brien T. Kevin, Langley Research Center, and United States. Army Aviation Research and Technology Activity., eds. Strain energy release rate analysis of delamination in a tapered laminate subjected to tension load. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Demirer, Halil. Glass fibre coatings based on polyimide-silica hybrids for use in epoxy matrix composites. 1998.

Woo, Monica Soon-wei. Effect of the interface on the moisture absorption behaviour of glass and carbon fibre reinforced epoxy. 1985.

C, Chamis C., Minnetyan L, and United States. National Aeronautics and Space Administration., eds. Prediction of composite laminate fracture: Micromechanics and progressive fracture. [Washington, D.C: National Aeronautics and Space Administration, 1996.

Jian, Zhang. Evaluation of an epoxy resin containing a carboxylic acid terminated fluoroligomer for use as matrix for glass fibre composites. 1993.