气动补偿空速管的研究与发展  

THE RESEARCH AND DEVELOPMENT OF THE AERODYNAMIC COMPENSATED PITOT-STATIC TUBE

作　　者：武文康[1] 屠兴[1] 

机构地区：[1]西北工业大学

出　　处：《气动实验与测量控制》1993年第4期11-16,共6页

摘　　要：气动补偿空速管是与飞行安全性和飞机飞行的高度分层密切相关的重要器件,在改进现役飞机和设计新机空速系统中起着重要作用。本文依据多年来大量的气动计算和风洞实验所得到的结果,叙述了气动补偿空速管的原理、分类、设计思想、特点、风洞校准、气动计算、使用和发展等情况。Aerodynamic compensated Pitot-static tube is a main part for flight safty of an aircfaft and is close related to the distance between flightlayers.It plays an important role in improving the performance of an air-craft used and designing a pitot-static pressure system for a new aircraft.Thispaper describes the principle,type,design idea,characteristics,wind tunnelcalibration,aerodynamic calculation use and development of the aerodynamiccompensated pitot-static tube from the results obtained from the aerodynamiccalculation and wind tunnel tests in reeentyears.

关 键 词：空速管 气动补偿 前体补偿 飞机 

分 类 号：V241.432[航空宇航科学与技术—飞行器设计]