helicopter tail rotor

基本解釋

This paper also presents the fatigue testing of helicopter composite tail rotor blade.
本文主要研究這些缺陷對復(fù)合材料槳葉疲勞壽命的影響。
This paper introduces a method of making selection of helicopter tail rotor parameter optimization using computer optimum techniques.
本文介紹采用計算機(jī)優(yōu)化技術(shù)進(jìn)行直升機(jī)尾槳參數(shù)優(yōu)化選擇的方法。
Chaos characteristics of the aerodynamic noise are discussed and the aeroacoustic noise signals on helicopter scissors tail rotor is analyzed by the chaos theory.
研究剪刀式尾槳氣動噪聲的混沌特性，并應(yīng)用混沌理論進(jìn)行了直升機(jī)尾槳氣動噪聲信號分析。