摘要
研究了人头颈部的气动特性和生物力学特性,提出人头颈部受到高速气流吹袭时,对气动阻力的耐受限值为2.452kN,对气动升力的耐受限值为1.358kN,对气动侧力的耐受限值为0.169kN,并给出了人头颈部高速气流吹袭的耐限曲线。不论乘员在何种姿势下弹射,作用在头颈部的气动力不超过以上数值才可免遭高速气流吹袭造成的损伤。
To provide parameters for designers of open type escape system in an aircraft, aerodynamic and biomechanical characteristics of human head neck region was studied and analysed.The results show that tolerance limit of human head neck region are 2.452kN, 1.358 kN and 0.169kN to aerodynamic drag,aerodynamic lift,and aerodynamic side force respectively during high speed windblast.Meanwhile the curve of tolerance limit to high speed windblast is given. Regardless of crewman posture during ejection, human head neck region is free from windblast injury unless the aerodynamic force exerted on the head neck region is within the above mentioned value.
出处
《航天医学与医学工程》
CAS
CSCD
1997年第1期6-10,共5页
Space Medicine & Medical Engineering
关键词
弹射
气流吹袭
航空安全
头颈
生理耐受限值
ejection windblast aviation safety head neck physiological tolerance limits impact damage