Residual strength
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The concept Residual strength represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
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Residual strength
Resource Information
The concept Residual strength represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
- Label
- Residual strength
- Source
- nasat
23 Items that share the Concept Residual strength
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- The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles
- A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications
- A progressive damage methodology for residual strength predictions of center-crack tension composite panels
- A progressive damage methodology for residual strength predictions of notched composite panels
- Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure
- Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure
- Boeing/NASA composite components flight service evaluation
- Damage characteristics and residual strength of composite sandwaich panels impacted with and without compression loading : presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, session no. 15-damage tolerance : Long Beach, California, April 20-23, 1998
- Determination of residual stress in composite materials using ultrasonic waves : NASA contract # NAG3-1716
- Isothermal fatigue, damage accumulation, and life prediction of a woven PMC
- Long-term environmental effects and flight service evaluation of composite materials
- Nonlinear response and residual strength of damaged stiffened shells subjected to combined loads
- Nonlinear response and residual strength of damaged stiffened shells subjected to combined loads
- Progressive Damage Analysis of Laminated Composite (PDALC) : a computational model implemented in the NASA COMET finite element code
- Progressive Damage Analysis of Laminated Composite (PDALC)--a computational model implemented in the NASA COMET finite element code
- Progressive damage analysis of laminated composite (PDALC) : (a computational model implemented in the NASA COMET finite element code) version 2.0
- Relevance of impacter shape to nonvisible damage and residual tensile strength of a thick graphite/epoxy laminate
- Residual strength analyses of riveted lap-splice joints
- Residual strength analyses of riveted lap-splice joints
- Simulation studies for surfaces and materials strength : semiannual progress report for cooperative agreement NCC2-297 for the period November 1, 1986 - April 30, 1987
- Stressed oxidation of C/SiC composites
- Stressed oxidation of C/SiC composites
- Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/resource/iJvQ9GXr0pw/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/iJvQ9GXr0pw/">Residual strength</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>