1-24 of 121 Books
Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections
Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections
By J. Scott Collins
Test report--fault current through graphite filament reinforced plastic
Test report--fault current through graphite filament reinforced plastic
By R. W. Evans
Advanced composites design data for spacecraft structural applications
Advanced composites design data for spacecraft structural applications
By R. Doug Holmes
Free vibrations of thin-walled semicircular graphite epoxy composite frames
Free vibrations of thin-walled semicircular graphite epoxy composite frames
By Huey D. Carden
Stacking-sequence optimization for buckling of laminated plates by integer programming
Stacking-sequence optimization for buckling of laminated plates by integer programming
By Raphael T. Haftka
Progressive fracture of fiber composite build-up structures
Progressive fracture of fiber composite build-up structures
By Pascal K. Gotsis
Flight service evaluation of advanced composite ailerons on the L-1011 transport aircraft
Flight service evaluation of advanced composite ailerons on the L-1011 transport aircraft
By R. H. Stone
Mixed-mode cyclic debonding of adhesively bonded composite joints
Mixed-mode cyclic debonding of adhesively bonded composite joints
By Mohammad Ali Rezaizadeh
Effect of low-speed impact damage and damage location on behavior of composite panels
Effect of low-speed impact damage and damage location on behavior of composite panels
By Dawn C. Jegley
Effects of through-the-thickness stitching on impact and interlaminar fracture properties of textile graphite/epoxy laminates
Effects of through-the-thickness stitching on impact and interlaminar fracture properties of textile graphite/epoxy laminates
By Suresh K. Sharma
Finite-element vibration analysis and modal testing of graphite epoxy tubes and correlation between the data
Finite-element vibration analysis and modal testing of graphite epoxy tubes and correlation between the data
By Barmac K. Taleghani
Thermal output of WK-type strain gauges on various materials at cryogenic and elevated temperatures
Thermal output of WK-type strain gauges on various materials at cryogenic and elevated temperatures
By Matthew K. Kowalkowski
A new merit function for evaluating the flaw tolerance of composite laminates
A new merit function for evaluating the flaw tolerance of composite laminates
By Martin M. Mikulas
Analysis of static contact in laminated composite plates using damage mechanics
Analysis of static contact in laminated composite plates using damage mechanics
By Allen, David H.
Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads
Progressive fracture of fiber composite thin shell structures under internal pressure and axial loads
By Pascal K. Gotsis
Structural testing of a stitched/resin film infused graphite-epoxy wing box
Structural testing of a stitched/resin film infused graphite-epoxy wing box
By Dawn C. Jegley
Flight service evaluation of composite helicopter components
Flight service evaluation of composite helicopter components
By Melvin J. Rich
Unlined reusable filament wound composite cryogenic tank testing
Unlined reusable filament wound composite cryogenic tank testing
By A. W. Murphy
Buckling behavior of long anisotropic plates subjected to combined loads
Buckling behavior of long anisotropic plates subjected to combined loads
By Michael P. Nemeth
Acoustic method of damage sensing in composite materials, final report for contract NAS8-38609, delivery order 99
Acoustic method of damage sensing in composite materials, final report for contract NAS8-38609, delivery order 99
By Gary L. Workman
Buckling behavior of long symmetrically laminated plates subjected to shear and linearly varying axial edge loads
Buckling behavior of long symmetrically laminated plates subjected to shear and linearly varying axial edge loads
By Michael P. Nemeth
Compression response of a sandwich fuselage keel panel with and without damage
Compression response of a sandwich fuselage keel panel with and without damage
By David M. McGowan