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Regeneratively cooled scramjet engine start-up phase heat transfer characteristics of
Author: YangXiaoZhu
Tutor: WangZhenGuo
School: National University of Defense Science and Technology
Course: Aeronautical and Astronautical Science and Technology
Keywords: Regenerative cooling Scramjet engine start-up phase Unsteady heat transfer Supercritical kerosene Two-phase flow instabilities
CLC: V231.1
Type: Master's thesis
Year: 2011
Downloads: 52
Quote: 0
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Abstract
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CLC: > Aviation, aerospace > Aviation > Aero-engine ( propulsion system ) > Engine theory > Thermodynamics, heat transfer
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