Books on the topic 'Composite beam'

Electron beam curing of composites. Munich: Hanser Publications, 2010.

Martin, Roderick H. Evaluation of the split cantilever beam for mode III delamination testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

W, Nixon Mark, Rehfield Lawrence W, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Comparison of composite rotor blade models: A coupled-beam analysis and an MSC/NASTRAN finite-element model. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

Ragon, Scott A. Optimization of composite box-beam structures including effects of subcomponent interaction. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University, 1995.

Center, Langley Research, ed. Friction and wear behavior of aluminum and composite I-beam stiffened airplane skins. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Center, Langley Research, ed. Friction and wear behavior of aluminum and composite I-beam stiffened airplane skins. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Center, Langley Research, ed. Friction and wear behavior of aluminum and composite I-beam stiffened airplane skins. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Lai, Zhichao. Composite special moment frames: Wide flange beam to concrete-filled steel column connections. Reston, Virginia: American Society of Civil Engineers, 2020.

D, Roberts Gary, Papadopoulos Demetrios S, and United States. National Aeronautics and Space Administration., eds. The effect of contact stresses in four-point bend testing of graphite/epoxy and graphite/PMR-15 composite beams. [Washington, DC: National Aeronautics and Space Administration, 1992.

D, Roberts Gary, Papadopoulos Demetrios S, and United States. National Aeronautics and Space Administration., eds. The effect of contact stresses in four-point bend testing of graphite/epoxy and graphite/PMR-15 composite beams. [Washington, DC: National Aeronautics and Space Administration, 1992.

Wolff-Fabris, Felipe, Volker Altstädt, Ulrich Arnold, and Manfred Döring. Electron Beam Curing of Composites. München: Carl Hanser Verlag GmbH & Co. KG, 2010. http://dx.doi.org/10.3139/9783446433465.

Fan, Chun Keung Roger. Buckling in continuous composite beams. [s.l.]: typescript, 1990.

Molenstra, Nadia Julia. Ultimate strength of composite beams. [s.l.]: typescript, 1990.

United States. National Aeronautics and Space Administration., ed. Flutter analysis of composite box beams. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Kissane, Robert J. Lateral restraint of non-composite beams. Albany, NY: New York State Dept. of Transportation, Engineering Research and Development Bureau, 1985.

Hughes, G. Longitudinal shear in composite concrete bridge beams. Crowthorne: Transport and Road Research Laboratory, 1987.

Hughes, G. Longitudinal shear in composite concrete bridge beams. Crowthorne: Transport and Road Research Laboratory, 1986.

Darwin, David. Steel and composite beams with web openings: Design of steel and composite beams with web openings. Chicago, Ill: American Institute of Steel Construction, 1990.

N, Murthy P. L., and United States. National Aeronautics and Space Administration., eds. Design procedures for fiber composite box beams. [Washington, D.C.]: National Aeronautics and Space Administration, 1988.

Ghorashi, Mehrdaad. Statics and Rotational Dynamics of Composite Beams. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-14959-2.

Shiming, Chen. Instability of composite beams in hogging bending. [s.l.]: typescript, 1992.

Ohseop, Song, ed. Thin-walled composite beams: Theory and application. Dordrecht, The Netherlands: Springer, 2006.

Librescu, Liviu. Thin-walled composite beams: Theory and application. Dordrecht: Springer, 2006.

W, Hyer M., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Large deformation dynamic bending of composite beams. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Farley, Gary L. Energy-absorption capability of composite tube and beams. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

Farley, Gary L. Energy-absorption capability of composite tube and beams. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

M, Jones Robert, United States. Army Aviation Research and Technology Activity., and Langley Research Center, eds. Energy-absorption capability of composite tube and beams. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

Center, Lewis Research, ed. Free vibrations of delaminated beams. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1992.

Banks, H. Thomas. On damping mechanisms in beams. Hampton, Va: ICASE, 1989.

Thompson, P. Buckling of composite beams (CDDF final report - project no. 91-20). Huntsville, Ala: George C. Marshall Space Flight Center, 1994.

Rosado, Pablo Rodríguez. Design of multiple-ply laminated composite tapered beams. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.

Rosado, Pablo Rodríguez. Design of multiple-ply laminated composite tapered beams. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.

George C. Marshall Space Flight Center., ed. Design of multiple-ply laminated composite tapered beams. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.

Rodriguez, P. Design of multiple-ply laminated composite tapered beams. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1993.

Henry, Desmond Paul. Development of BEM for ceramic composites. Buffalo, N.Y: Calspan-UB Research Center, 1991.

Farley, Gary L. A method of predicting the energy-absorption capability of composite subfloor beams. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

Lawson, R. M. Design for openings in the webs of composite beams. London: Construction Industry Research & Information Association, 1987.

B, Manbeck H., and Forest Products Laboratory (U.S.), eds. Performance of Red Maple glulam timber beams. Madison, WI. (One Gifford Pinchot Dr., Madison, 53705-2398): U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1993.

Huang, Dong-jie. Composite beams: Reliability and longitudinal shear resistance with profiled sheeting. [s.l.]: typescript, 1994.

Centre, Bhabha Atomic Research, ed. Development of electron beam grafted co-polymer membranes for recovery of uranium from seawater: Process parameter standardization. Mumbai: Bhabha Atomic Research Centre, 2005.

Thompson, P. Buckling of composite beams: CDDF final report : project no. 91-20. MSFC, Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 1994.

George C. Marshall Space Flight Center., ed. Buckling of composite beams: CDDF final report : project no. 91-20. MSFC, Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 1994.

Paul, Henry Desmond, and United States. National Aeronautics and Space Administration., eds. Development of BEM for ceramic composites: Final report. Buffalo, N.Y: Calspan-UB Research Center, 1993.

P, Henry D., and United States. National Aeronautics and Space Administration., eds. Development of BEM for ceramic composites: Final report. Buffalo, N.Y: Calspan-UB Research Center, 1993.

I, Kachlakev Damian, and Oregon. Dept. of Transportation. Research Group., eds. Behavior of FRP composite-strengthened beams under static and cyclic loading. Salem, OR: Oregon Dept. of Transportation, Research Group, 2001.

Hodges, Dewey H. Modeling of composite beams and plates for static and dynamic analysis. Atlanta, Ga: School of Aerospace Engineering, Georgia Institute of Technology, 1990.

Center, Langley Research, ed. A higher-order bending theory for laminated composite and sandwich beams. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Center, Langley Research, ed. A higher-order bending theory for laminated composite and sandwich beams. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

United States. National Aeronautics and Space Administration., ed. Modeling of composite beams and plates for static and dynamic analysis. [Washington, DC: National Aeronautics and Space Administration, 1993.

Zafer, Gürdal, and United States. National Aeronautics and Space Administration., eds. Compression of thick laminated composite beams with intitial impact-like damage. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1992.