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>The effect of nose geometry on the aerothermodynamic environment of shuttle entry configurations
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The effect of nose geometry on the aerothermodynamic environment of shuttle entry configurations
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机译:机头几何形状对航天飞机进入结构的空气动力学环境的影响
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摘要
The effect was studied of nose geometry on the transition criteria for the windward boundary layer, on the extent of separation, on the heat transfer perturbation due to the canopy, and on the surface pressure and the heat transfer in the separated region. The data for each of these problems is analyzed. A literature review that concentrates on separation and the leeward flow-field is presented.
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