極超音速飛翔体周りに生じる温度分布の可視化法

抄録

A method for visualizing qualitative temperature distributions around hypersonic vehicles is suggested. As an example of this method, a temperature layer over a slightly blunted wedge is visualized. The photograph indicates that there exists a radiation contrast along the wedge surface. From this, it is considered that the present method may be useful for visualizing gas temperature distributions around hypersonic models.