• Proceedings of the KSME Conference
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• 2004.04a
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• pp.716-721
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• 2004

In this study, dome port bringing up for discussion where the ramjet occurs in flying it presents the tendency of distribution of thermal contour due to temperature and pressure. It is assumed that the material of ramjet is steel for the ease of result analysis. It applied matrial property which it follows by temperature and input boundary condition that changing temperature and pressure on each region by time difference for transient analysis. Thermal analysis region is decided until dome port part is separated and operate analysis in 0.5 second. Finally we draw tendency of thermal contour in ramjet dome port part by temperature and pressure.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2004.10a
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• pp.223-226
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• 2004

The objectives of this study are to evaluate mechanical properties of glass ceramic for dome port cover material o( the ramjet. Candidate material for dome port cover of the ramjet is selected the machinable glass ceramic(MACOR glass-filled ceramic, Corning Glass Works, code 9658). Static and dynamic fracture toughness tests were performed to evaluate the apparent fracture toughness of notched specimen.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• v.y2005m4
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• pp.112-115
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• 2005

The objectives of this study are to evaluate the dynamic fracture toughness of advance glass ceramics(MACOR glass-filled ceramic, Corning Glass Works) for dome port cover of the ramjet. Static and dynamic fracture toughness tests are performed using strain gage method in the variation of notch radii.