Add to ORKGHeated structural parts alter their shape. Anything which hinders free heat expansion will give rise to heat stresses. Design rules are thus obtained for the heated walls themselves as well as for the adjoining parts. An important guiding principle is that of designing the heat-conducting walls as thin as possible
The materials of the combustion chamber wall of rocket engines have to withstand extreme thermal and...
The development of a holistic, effective, and scalable structure of economic management, as well as ...
Modern jet engine design imposes extremely high loadings and temperatures on hot section components....
The power and heat-stress conditions of geometrically similar engines are discussed. The advantages ...
The gas expansion process that takes place in a piston cylinder assembly have been used in numerous ...
Heat losses are a major limiting factor for the efficiency of internal combustion engines. Furthermo...
This paper deals with a structural stress analysis of the cylinder head assembly of the C/28 series ...
Uninsulated structures fabricated from carbon or silicon-based materials, which are allowed to becom...
In this paper is presented the calculus mode of thermal transmission in a cylinder cover of an inter...
Factors that affect heat transfer in the linered aluminium engine block are examined to determine th...
NASA sponsored the Turbine Engine Hot Section (HOST) project to address the need for improved durabi...
Research and plans concerning aircraft gas turbine engine hot section durability problems were discu...
Abstract : Modern foreign and domestic scientific literature has extensive information on the creat...
Aircraft structure subjected to elevated temperature and acoustic loading present a challenging desi...
In Sterling-cycle heat engine, pneumatic system is used to drive displacer/regenerator, eliminating ...
The materials of the combustion chamber wall of rocket engines have to withstand extreme thermal and...
The development of a holistic, effective, and scalable structure of economic management, as well as ...
Modern jet engine design imposes extremely high loadings and temperatures on hot section components....
The power and heat-stress conditions of geometrically similar engines are discussed. The advantages ...
The gas expansion process that takes place in a piston cylinder assembly have been used in numerous ...
Heat losses are a major limiting factor for the efficiency of internal combustion engines. Furthermo...
This paper deals with a structural stress analysis of the cylinder head assembly of the C/28 series ...
Uninsulated structures fabricated from carbon or silicon-based materials, which are allowed to becom...
In this paper is presented the calculus mode of thermal transmission in a cylinder cover of an inter...
Factors that affect heat transfer in the linered aluminium engine block are examined to determine th...
NASA sponsored the Turbine Engine Hot Section (HOST) project to address the need for improved durabi...
Research and plans concerning aircraft gas turbine engine hot section durability problems were discu...
Abstract : Modern foreign and domestic scientific literature has extensive information on the creat...
Aircraft structure subjected to elevated temperature and acoustic loading present a challenging desi...
In Sterling-cycle heat engine, pneumatic system is used to drive displacer/regenerator, eliminating ...
The materials of the combustion chamber wall of rocket engines have to withstand extreme thermal and...
The development of a holistic, effective, and scalable structure of economic management, as well as ...
Modern jet engine design imposes extremely high loadings and temperatures on hot section components....