本文在平面截面的假定下，以幂次自模拟解为基础，提出了高超音速气流绕一般细长（辶回）转体流动的普遍线性化理论。
On the basis of a self-similar solution as well as of the assumption, of the "Transverse Motion", a general linear theory on hypersonic flow over a general slender body is set up in this paper.
分别用幂法和QR法计算结构的第一和所有自振频率。
The first natural frequency and all natural frequencies areobtained by the power method and the QR method, respectively.
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