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提出了无纵向温度变形的复合材料管子铺层设计的一种方法。通过对三类碳纤维／ 环氧复合材料的管子的实例计算表明：高模碳纤维，而不是极高模量碳纤维，更适合于航天结构的应用。
A method for design of composite pipe ply without longitudinal temperature deformation is proposed. The calculation of three types of carbon fiber / epoxy composite pipe shows that high modulus carbon fibers, rather than very high modulus carbon fibers, are more suitable for aerospace applications.