目的比较和分析Rpl32和Rpl13作为单内参基因与两者作为双内参基因,用于检测大鼠挫伤肌肉组织中TAB2 m RNA表达量的结果。方法 78只SD大鼠,随机分为正常对照组(1组)和肌肉损伤组(12组)。采用自由落体法制作大鼠肌肉挫伤模型,分别于4h^48...目的比较和分析Rpl32和Rpl13作为单内参基因与两者作为双内参基因,用于检测大鼠挫伤肌肉组织中TAB2 m RNA表达量的结果。方法 78只SD大鼠,随机分为正常对照组(1组)和肌肉损伤组(12组)。采用自由落体法制作大鼠肌肉挫伤模型,分别于4h^48h之间12个时间点取肌肉组织,提取总RNA、合成c DNA、采用real-time q PCR法,以Rpl32和Rpl13作为单独内参基因和二者作为双内参基因检测大鼠肌肉挫伤组织中TAB2 m RNA相对表达量,并计算检测结果的变异系数。结果以Rpl32或Rpl13单独作为内参基因或作为双内参基因,TAB2 m RNA表达随损伤时间总体均呈现降低的变化规律,但使用单内参基因在24h和32h出现极高值,而用双内参基因计算未出现极值,且各结果的变异系数均较小。结论 Rpl32和Rpl13作为双内参基因用于计算TAB2 m RNA相对表达量,可提高分析结果的准确性,在相关实验中建议选择使用。展开更多
A study is conducted on the feasibility of helicopter ground and air resonanceby using actively controlled tabs mounted at the trailing edge of an aerofoil. A method isdeveloped to obtain the optimal feedback control ...A study is conducted on the feasibility of helicopter ground and air resonanceby using actively controlled tabs mounted at the trailing edge of an aerofoil. A method isdeveloped to obtain the optimal feedback control law through constructing a referencemodel according to requirements of stability levels in the modal space. The effects of rotorspeed and length and location of tabs on the control law are analyzed, and it is found possible that a controller can be designed into constant feedback gain against rotor speed andto feed back only to the dominant system states to eliminate the unstable range of rotorspeed.展开更多
文摘目的比较和分析Rpl32和Rpl13作为单内参基因与两者作为双内参基因,用于检测大鼠挫伤肌肉组织中TAB2 m RNA表达量的结果。方法 78只SD大鼠,随机分为正常对照组(1组)和肌肉损伤组(12组)。采用自由落体法制作大鼠肌肉挫伤模型,分别于4h^48h之间12个时间点取肌肉组织,提取总RNA、合成c DNA、采用real-time q PCR法,以Rpl32和Rpl13作为单独内参基因和二者作为双内参基因检测大鼠肌肉挫伤组织中TAB2 m RNA相对表达量,并计算检测结果的变异系数。结果以Rpl32或Rpl13单独作为内参基因或作为双内参基因,TAB2 m RNA表达随损伤时间总体均呈现降低的变化规律,但使用单内参基因在24h和32h出现极高值,而用双内参基因计算未出现极值,且各结果的变异系数均较小。结论 Rpl32和Rpl13作为双内参基因用于计算TAB2 m RNA相对表达量,可提高分析结果的准确性,在相关实验中建议选择使用。
文摘A study is conducted on the feasibility of helicopter ground and air resonanceby using actively controlled tabs mounted at the trailing edge of an aerofoil. A method isdeveloped to obtain the optimal feedback control law through constructing a referencemodel according to requirements of stability levels in the modal space. The effects of rotorspeed and length and location of tabs on the control law are analyzed, and it is found possible that a controller can be designed into constant feedback gain against rotor speed andto feed back only to the dominant system states to eliminate the unstable range of rotorspeed.
