Computer Code for Thermal Analysis of Rocket Motors - Riise, Jørn Arnold Kvistad
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Heat transfer in rocket motors is being increasingly investigated to better understand the physical material changes during the operational time of the motor. Material durability is important since the motor structure requires strength and maneuverability to bring off a successful flight. A computer program that is simulating this material behavior is a useful tool for the rocket motor designer. Rocket motor designs can then be tested and evaluated before an actual firing test is required.

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Produktbeschreibung
Heat transfer in rocket motors is being increasingly investigated to better understand the physical material changes during the operational time of the motor. Material durability is important since the motor structure requires strength and maneuverability to bring off a successful flight. A computer program that is simulating this material behavior is a useful tool for the rocket motor designer. Rocket motor designs can then be tested and evaluated before an actual firing test is required.
Autorenporträt
Jørn A. K. Riise (born 1984) submitted this work as a conclusion of a Master of Science degree in Engineering & ICT with specialisation in the field of energy and process engineering. Since graduating from the Norwegian University of Science and Technology in Trondheim, he has worked for a leading engineering company in the oil and gas industry.