scholarly journals Sandstone dikes in dolerite sills: Evidence for high-pressure gradients and sediment mobilization during solidification of magmatic sheet intrusions in sedimentary basins

Geosphere ◽  
2010 ◽  
Vol 6 (3) ◽  
pp. 211-224 ◽  
Author(s):  
Henrik Svensen ◽  
Ingrid Aarnes ◽  
Yuri Y. Podladchikov ◽  
Espen Jettestuen ◽  
Camilla H. Harstad ◽  
...  
2002 ◽  
Vol 3 (3) ◽  
pp. 245-249 ◽  
Author(s):  
Stephen R. Grobmyer ◽  
Dennis Graham ◽  
Murray F. Brennan ◽  
Daniel Coit

1964 ◽  
Vol 86 (4) ◽  
pp. 729-735 ◽  
Author(s):  
G. A. Samara ◽  
A. Henius ◽  
A. A. Giardini

A study of operational characteristics and stress distribution in a large volume hexahedral apparatus has been made. Pyrophyllite containers with integral preformed gaskets were found to be superior to plain blocks. Pregasketing reduced material flow and sample deformation, increased by over 100 percent the central region of the container over which little or no deformation occurs, and greatly increased anvil life. Even so, large pressure gradients still existed within the container. These gradients become more severe the higher the pressure. Pressure efficiency and distribution were appreciably changed by varying the length and thickness of preformed gaskets. Built-in metal intensifiers increased pressure efficiency by up to 30 percent. The inclusion of a metal heater tube had no measurable influence on pressure gradients. Cycling decreased the applied load required to reach a given pressure only if the load was not allowed to fall below a certain minimum. This is attributed to the ability of pyrophyllite to remain static while supporting large stress gradients.


1998 ◽  
Vol 38 (3) ◽  
pp. 325-329 ◽  
Author(s):  
S Günter ◽  
S.D Pinches ◽  
A Gude ◽  
K Hallatschek ◽  
K Lackner ◽  
...  

Author(s):  
Roberto Ciorciari ◽  
Ilker Kirik ◽  
Reinhard Niehuis

In modern low pressure turbines the efforts to increase aerodynamic blade loading by increasing blade pitch and optimising midspan performance in order to reduce weight and complexity can produce increased losses in the endwall region. Airfoils of high flow turning and high pressure gradients between the blades generate strong secondary flows which impair the global aerodynamic performance of the blades. In addition, the unsteady incoming wakes take influence on transition phenomena on the blade surfaces and the inlet boundary layer, and consequently affect the development and the evolution of the secondary flows. In this paper the T106 cascade is used to identify the effect of unsteady wakes on the development of secondary flows in a turbine cascade. Numerical and experimental results are compared at different flux coefficients and Strouhal numbers, the relative differences and similarities are analysed.


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