Development of energy dissipating plastic honeycomb Quarterly progress report, 1 Aug. - 31 Oct. 1966
Manufacturing modifications, and glass filler additions for dip resin used in honeycomb structures
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Manufacturing modifications, and glass filler additions for dip resin used in honeycomb structures
Photoelastoplastic method using creep and stress characteristics of epoxy resins under thermal cycle, discussing stress-strain behavior
Fracture theory for amorphous high polymers below glass transition temperature, considering viscoelastic effects on structural defect stress concentration
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Small units of standard glass apparatus held together by short lengths of transparent heat-shrinkable polyolefin tubing. The tubing is shrunk over glass O-ring type connectors having O-rings but no lubricant.
Equations for solving initial and boundary value problems in elastoplastic flow in longitudinally stressed, axisymmetric notched rods
Axial slit effects on residual tensile strengths of polyethylene terephthalate film and fabric cylindrical shells
Bending analysis of elastoplastic circular plates for small deflection and axisymmetric loadings and support conditions, based on Kirchhoff hypothesis
Elastoplastic flow equations character in three independent variables, noting solution methods for initial and boundary value problems
Metallic coating directly sprayed on electronic modules provides simple and reliable lightweight protection against radio frequency interference. A plasma arc may be used. Aluminum and copper are the most effective metals.
Hexagonal and nonhexagonal cell phenolic honeycomb structures as energy dissipating material for spacecraft construction
Analysis of supported circular plate under impulsive loading
Plane strain and stress compared for elastoplastic cracked plate in work hardening tension
Elastoplastic flow equations formulation, inverting flow rule to relate stress rates to strain rates and instantaneous stresses, noting Navier equations
Dies of a phenolic molding compound with chopped glass fibers as fill material possess a flexural strength of 20,000 psi and a compressive strength of 28,500 psi.
Strain gage is installed during molding of composite and utilizes the adhesive properties of the matrix resin in the composite to bond the strain gage in place. Gages thus embedded provide data at all temperatures that the matrix can withstand.
Mismatch and weld sinkage problems of pressure vessel geometric discontinuities studied in design graphs and test program
Electron bombardment produced clustered displacements, paired vacancies and interstitial atoms in Si, discussing possible mechanism for developing defects