Investigation of strength of isolated vertebrae, phase IV Final technical report, 29 Oct. 1965 - 28 Oct. 1966
Dynamic strength measurements of human vertebrae under axial compression
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Dynamic strength measurements of human vertebrae under axial compression
Safety design for high strength low toughness materials assumed to have hidden flaws, formulating stress intensity factor for fracture mechanics
Texture strength and fracture toughness of titanium alloy sheet biaxial stress fields at room and cryogenic temperatures
Stiffness and strength analyses on composite cross-ply and helical wound cylinders and flat laminate structures
Results are presented of rapid-heating tests of 17-7 PH and 12 MoV stainless-steel sheet heated to failure at temperature rates from about 1 F to 170 F per second under constant-load conditions. Yield and rupture strengths obtained from rapid-heating tests are compared with yield and tensile strengths obtained from short-time elevated-temperature tensile tests (30-minute exposure). A rate-temperature parameter was used to construct master curves from which yield and rupture stresses or temperatures can be predicted. A method for measuring strain by optical means is described.
Impact strength of titanium unaffected by heating time during vacuum heating
Strength characteristics of industrial melts of multicomponent titanium alloys with .03 to .075 aluminum content
The Urban Air Mobility Side-by-Side Test Stand (SBS) is a new capability for the National Aeronautics and Space Administration (NASA) to test the conceptual side-by-side rotorcraft configuration. This test stand enhances the experimental capabilities of the Revolutionary Vertical Lift Technology (RVLT) Project and is primarily designed to be tested in the U.S. Army’s 7-by 10-Foot Wind Tunnel at NASA Ames Research Center. One of the goals for the SBS is to identify the optimal degree of rotor overlap that will yield the best aerodynamic performance. The SBS has two counter-rotating, intermeshing rotors that can vary in lateral separation. The test stand can pitch nose up and nose down, with each rotor having the capability to be trimmed independently through cyclic and collective controls. Six-axis load cells and rotary torque sensors are placed underneath each rotor to measure the thrust, torque, and side force from each rotor system. This paper describes the mechanical design of the SBS and outlines the structural analyses conducted to ensure a safety factor of 4 for ultimate strength and 3 for yield strength during all experimental testing.
Mechanisms of strengthening and fracture in composite materials
Yielding behavior and dislocation motion in two phase crystalline solid
Yield stress of polymethyl methacrylate subjected to vacuum UV radiation is function of strain rate, tensile test temperature and irradiation dose
Elevated temperatures effect on sputtering yields of polycrystalline and single crystal metals, considering defect annealing and focused collision sequence
Lightweight magnesium alloys for cryogenic applications
Yield stress master curve for polymers below glass transition temperature
Linearity of mechanical behavior and applicability of yield stress master curve analyzed for various crystalline-type polymers
Temperature, time and loading conditions for adhesion or cohesion of structural metals in vacuum
Stress corrosion mechanism of titanium noting experimental conditions, results of chemical analyses, time factor, material resistance to crack formation, etc
Solvent system dissolves the solid curing agents used with polyurethane resins in adhesive systems. The system developed yields bond strengths comparable to 100 percent solid formulations. The optimum solvent chosen was a 55.5 percent solution in anhydrous tetrahydrofuran.