一种对流层软式飞艇设计体积估算方法的商榷  

Discussion about an Estimating-method for Troposphere Blimp Designing-volume

作　　者：张博[1] 王大华[1] 

机构地区：[1]海军工程大学,湖北武汉430033

出　　处：《航空计算技术》2008年第4期56-60,共5页Aeronautical Computing Technique

摘　　要：出于对对流层软式飞艇动态受力平衡的考虑,分别从一般情况、特定任务和限制飞艇地面净重(轻)情况三个角度分析,尝试建立了飞艇设计体积与携带燃油量的数学关系模型,并利用仿真曲线相交的方法,对飞艇设计体积进行区间估算,以此作为设计目标值的依据。By analyzing the situations of the general situation, specific tasks, restrictions of airship ground NW （Light） respectively, a mathematical model of the relationship between designing- volume and portable fuel is attempted to be built in consideration of troposphere blimp by the dynamic balance. Meanwhile the method of simulating- curves intersection is used to estimate interval designing-volume which is the basis of the design target.

关 键 词：对流层 软式飞艇 设计体积 估算方法 

分 类 号：V274[航空宇航科学与技术—飞行器设计]