Tomeki

Explore Books on
hole geometry (mechanics)

1-6 of 6 Books

View Analytical modeling of pressure wall hole size and maximum tip-to-tip crack length for perforating normal and oblique orbital debris impacts By William P. Schonberg

Analytical modeling of pressure wall hole size and maximum tip-to-tip crack length for perforating normal and oblique orbital debris impacts

Analytical modeling of pressure wall hole size and maximum tip-to-tip crack length for perforating normal and oblique orbital debris impacts

By William P. Schonberg

View Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application By Ali Abdul-Aziz

Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application

Design evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application

By Ali Abdul-Aziz

View Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control By Scott C. Asbury

Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control

Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control

By Scott C. Asbury

View Micromechanics of compression failures in open hole composite laminates By Eunice Gail Guynn

Micromechanics of compression failures in open hole composite laminates

Micromechanics of compression failures in open hole composite laminates

By Eunice Gail Guynn

View Standard methods for open hole tension testing of textile composites By M. A. Portanova

Standard methods for open hole tension testing of textile composites

Standard methods for open hole tension testing of textile composites

By M. A. Portanova

View Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades By V. K. Garg

Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades

Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades

By V. K. Garg