Compression tests on integrally stiffened cylinders
Compression tests on integrally stiffened cylinders - determination of loads and stresses associated with general and local instability
LOAD DISTRIBUTION↗
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Linear Aerodynamic Loads on Cone-Cylinders at Mach Numbers from 0.7 to 2.0
Linear aerodynamic loads for cone-cylinder configurations in trisonic range
CYLINDER↗
Experimental investigation of the stability of monocoque domes subjected to external pressure.
Fabrication, testing and experimental results for rigid-vinyl plastic monocoque domes subjected to external pressure loads
SPHERICAL SHELL↗
Instability of cylindrical shells subjected to axisymmetric moving loads.
Donnell-type nonlinear theory for instability of cylindrical shell subjected to axisymmetric moving loads with constant velocity
LAPLACE TRANSFORM↗
Structural weight and cost comparison of large space structures employing beryllium-aluminum alloys.
Axially loaded cylindrical structures analyzed for optimum weight construction consistent with cost constraint, emphasizing beryllium-aluminum alloys
ALUMINUM ALLOY↗
On some solutions of ring shells.
Hollow metallic O rings used for sealing as thin shells under axisymmetric loading
AXISYMMETRIC DEFORMATION↗
An asymptotic analysis for large deflections of pressurized shallow spherical membrane shells.
Large deflections of symmetrically loaded shallow membrane shells of revolution, considering existence of boundary layer near edges and using asymptotic analysis
ASYMPTOTIC METHOD↗
Instability of cylindrical shells subjected to axisymmetric moving loads.
Donnell-type nonlinear theory for instability of cylindrical shell subjected to axisymmetric moving loads with constant velocity
LAPLACE TRANSFORM↗
Experimental studies of current distributions and radiation patterns of a resistively loaded V-antenna at quarter scale for a radio astronomy Explorer satellite Final report
Current distributions and radiation patterns of resistively loaded V-antenna at quarter scale for radio astronomy Explorer satellite
ANTENNA↗
Solution of the problem of the cyclically symmetrical deformation of a conic shell in degenerate hypergeometrical functions
Calculation of forces, moments, strains, and displacements occurring in deformation of conic shell under action of force load and nonuniform heating - hypergeometrical functions
HYPERGEOMETRIC FUNCTION↗
An analysis of the elastic behavior of a capacitance load cell.
Elastic behavior of load cell operating on variable capacitance principle designed to fit spaces restricted in one dimension
LOAD DISTRIBUTION↗
Initial post-buckling behavior of toroidal shell segments.
Initial postbuckling behavior of double curvature shell segments under several loading conditions determined, using Koiter theory
ELASTIC BUCKLING↗
Large stiffened cylinder weight - Cost comparisons between Be-38 percent Al and other materials.
Axially loaded cylindrical structures analyzed for optimum weight construction consistent with cost constraint, emphasizing beryllium-aluminum alloys
ALUMINUM ALLOY↗
Stress intensity factors for crackline-loaded edge-crack specimens.
Stress intensity analysis for flat plates loaded close to edge crackline, giving intensity dependence on crack length and specimen shape
STRESS ANALYSIS↗
Finite transform solution of the vibrating annular membrane.
Vibrating annular membrane problem, including load per unit area and asymmetry of load and vibration, using finite transform derivation
LOAD DISTRIBUTION↗
Effect of high vacuum on the fatigue properties of magnesium and two magnesium alloys.
High vacuum environment and vacuum outgassing time effects on magnesium alloys fatigue properties under constant load and reversed bending
LOAD DISTRIBUTION↗
An accurate solution of the gas lubricated, flat sector thrust bearing
A flat sector shaped pad geometry for gas lubricated thrust bearings is analyzed considering both pitch and roll angles of the pad and the true film thickness distribution. Maximum load capacity is achieved when the pad is tilted so as to create a uniform minimum film thickness along the pad trailing edge. Performance characteristics for various geometries and operating conditions of gas thrust bearings are presented in the form of design curves. A comparison is made with the rectangular slider approximation. It is found that this approximation is unsafe for practical design, since it always overestimates load capacity.
Etsion, I.↗