subsonic

过去分词:

动词过去分词: subsoiled

更多词形:

名词: subsoiler | 动词过去式: subsoiled | 动词过去分词: subsoiled | 动词现在分词: subsoiling | 动词第三人称单数: subsoils |

单词例句:

WT5BZ]The optimum design of Controlled Diffusion Airfoils (CDA) is one of the main research fields in subsonic and transonic profile design for multistage compressor.

可控扩散叶型(CDA)的优化设计是目前国外对亚音、跨音速压气机叶型研究的主要内容之一。

For several given types of inlet boundary layer, a numerical investigation on flow field of bowed stator vanes under two inlet subsonic Mach numbers was carried out.

摘要给定不同型式的进口边界层,在两种不同亚音速条件下对一平面扩压静叶栅的弯叶片流场进行了数值模拟。

The relevance functions between total pressure recover coefficient and the parameters( Mach number, angle of attack, flow coefficient, angle of sideslip) for subsonic submerged inlet in turbojet and turbofan engine were investigated.

摘要根据某埋入式进气道试验数据建立了计算埋入式亚声速进气道总压恢复系数的经验公式,表现为关于马赫数、量系数、角、滑角的函数。

A numerical calculative method of computing aerodynamic characteristics for sideslipping thin wings of arbitrary planform with dihedral in subsonic flow is presented in this paper.

本文利用变换坐标的方法,把处理来流平行于机翼对称面的涡格法推广到有侧滑的情况去.文中计算了亚音速流中侧滑薄翼的气动特性。

Aachen 1.5 stage low speed subsonic axial turbine was used as an example of maximizing 3D clocking benefits by applying edge matching.

以A achen 1.5级亚声轴流涡轮为例展示了该方法的实际过程和效果。

Neutrino is the most unstable elementary state particle in numerous subsonic atom particles.

摘要在众多的亚原子粒子家族中,中微子是最令人捉摸不定的基本态粒子。

The drag of aftbody keeps constant in low subsonic flow, but increases in transonic flow due to the shock wave.

在低亚音速范围,后 体阻力基本不变化,随着马赫数增加至跨音速,出现激波阻力。

The relevance functions between total pressure recover coefficient and the parameters (Mach number, angle of attack, flow coefficient, angle of sideslip) for subsonic submerged inlet in turbojet and turbofan engine were investigated.

摘要根据某埋入式进气道试验数据建立了计算埋入式亚声速进气道总压恢复系数的经验公式,表现为关于马赫数、流量系数、攻角、侧滑角的函数。

This program calculates the aerodynamic forces from take-off up to landing and through the subsonic, transonic, and supersonic speed regimes.

使用的计算方法是根据实验数据和经验公式。本程序可计算起飞到着 陆的气动力。