Add to ORKGTechnique computes stresses resulting from axisymmetric transient thermal loading in circular solid-propellant grain section with circular ports. Propellant is assumed to be linear, thermal rheologically simple, viscoelastic material; material properties are represented by exponential series in time
A number of numerical solution technologies were developed for advanced analysis capabilities involv...
Analytical stress solutions are presented for a metallic rocket motor case reinforced with a prestra...
Abstract: In the paper an initial attempt to the experimental analysis of viscous effects, character...
The earlier progress reports presented some essentials of model representation and a summary of som...
Analysis of viscoelastic materials under transient thermal conditions related to solid rocket propel...
Previous reports of this series have attempted to define some of the important parameters affecting ...
Mechanical properties of viscoelastic filled polymers strongly depend on temperature and strain rate...
Mechanical characterization of solid fuel propellants - stress-strain behavior of inert composite pr...
Research projects concerned with developing a theory of fracture of materials are discussed. The eff...
For structural integrity evaluation of solid propellant grains under ignition pressurization load, a...
Typical High Temperature Applications High Temperature Applications Demand High Performance Material...
Analysis of bond stress in viscoelastic case bonded solid propellant rocket assembly during thermal ...
The results are presented of a viscoplastic stress-strain analysis of a cylindrical thrust chamber u...
A three dimensional nonlinear viscoelastic constitutive model for the solid propellant is developed....
Composite rocket propellants (CRP) have an elastomer as binder for the solid fillers, which serve as...
A number of numerical solution technologies were developed for advanced analysis capabilities involv...
Analytical stress solutions are presented for a metallic rocket motor case reinforced with a prestra...
Abstract: In the paper an initial attempt to the experimental analysis of viscous effects, character...
The earlier progress reports presented some essentials of model representation and a summary of som...
Analysis of viscoelastic materials under transient thermal conditions related to solid rocket propel...
Previous reports of this series have attempted to define some of the important parameters affecting ...
Mechanical properties of viscoelastic filled polymers strongly depend on temperature and strain rate...
Mechanical characterization of solid fuel propellants - stress-strain behavior of inert composite pr...
Research projects concerned with developing a theory of fracture of materials are discussed. The eff...
For structural integrity evaluation of solid propellant grains under ignition pressurization load, a...
Typical High Temperature Applications High Temperature Applications Demand High Performance Material...
Analysis of bond stress in viscoelastic case bonded solid propellant rocket assembly during thermal ...
The results are presented of a viscoplastic stress-strain analysis of a cylindrical thrust chamber u...
A three dimensional nonlinear viscoelastic constitutive model for the solid propellant is developed....
Composite rocket propellants (CRP) have an elastomer as binder for the solid fillers, which serve as...
A number of numerical solution technologies were developed for advanced analysis capabilities involv...
Analytical stress solutions are presented for a metallic rocket motor case reinforced with a prestra...
Abstract: In the paper an initial attempt to the experimental analysis of viscous effects, character...