Synonyme wurden verwendet für:
Mechanics
Suche ohne Synonyme:
keywords:(Structural Mechanics)
Overview of the X-57 Structure Requirements, Modifications, and Airworthiness
Quantitative Fractography (QF) for FCG Analyses
Fokker 100 Fuselage Test: Lap Joints Exponential FCG Analysis
LCFLF Example Lifing Assessment (2004): F/A-18 Vertical Tail Attachment Stubs
Basic Information for Aircraft FCG Failure and Lifing Analyses
Aermacchi MB-326H Wing Spar (1990): Exponential FCG Analysis
Sikorsky S-61N Rotor Blade (1974): Exponential FCGR Analysis
EBA Example Lifing Assessment (2004): F/A-18 Horizontal Stabilator Spindles
Westland Lynx Rotor Hub (1998): Progression Marking LEFM Analysis
Cubic Rule Life Prediction Examples
P&W 125B Engine Bearing (1994): 2-Stage Exponential FCG Analysis
Development of Energy Absorbing Subfloor Concepts to Improve Crashworthiness of eVTOL Aircraft
LOADS@NASA" Leading Outstanding Aerospace Loads & Dynamics Solutions
Photogrammetry at the Landing and Impact Research Facility at NASA Langley Research Center
Advances in Low-Cost Manufacturing and Folding of Solar Sail Membrane
LSMS–L35, Miniature Crane for Payload Offloading and Manipulation: Development, and Application
Machine Learning Application on Aircraft Fatigue Stress Predictions
Some Remaining Research Challenges in Aerospace Structures
Enabling Enhanced Validation of Non-Destructive Evaluation Computational Models and Simulations
Initiation and Propagation of Skin/Stiffener Separation in Postbuckled Structures
Mass Mitigation in Structural Designs Via Dynamic Properties
Bistable Deployable Composite Booms With Parabolic Cross-Sections
Collection of Examples from Delamination Growth Analysis Performed over 24 Years
Crashworthiness of a Lift plus Cruise eVTOL Vehicle Design within Dynamic Loading Environments
Structural Response of a Stitched Composite Hybrid Wing Body Center Section
Arecibo Observatory Auxiliary M4N Socket Termination Failure Analysis
Fiber-Optic Strain-Based Deflection and Twist Sensing for a High-Aspect-Ratio Swept Wing
Estimation of Effective Elastic Properties of General Carbon/Carbon Honeycomb
Thin-Ply Composite Deployable Boom Structures For Solar Sails
Motion Magnification to Visualize the Modes of Space Structures
Aeroelastic Prediction Workshop #3 Welcome and Introduction
NASA Application of In-Space Structural Health Monitoring Technology