aerodynamic
英 [ˌeərəʊdaɪˈnæmɪk]
美 [ˌeroʊdaɪˈnæmɪk]
adj. (汽车等)流线型的,符合空气动力学原理的
复数:aerodynamics
BNC.22868 / COCA.17229
柯林斯词典
- ADJ-GRADED (汽车等)流线型的
If something such as a car has anaerodynamicshape or design, it goes faster and uses less fuel than other cars because the air passes over it more easily.- The secret of the machine lies in the aerodynamic shape of the frame.
该机器的精妙之处在于其构架呈流线型。
- The secret of the machine lies in the aerodynamic shape of the frame.
英英释义
adj
- designed or arranged to offer the least resistant to fluid flow
- a streamlined convertible
- of or relating to aerodynamics
双语例句
- The process of formation, aerodynamic coefficient and trajectory of EFP are calculated.
对所设计的EFP战斗部进行成型过程、气动力系数和飞行弹道计算。 - This article introduces the experimental investigations of aerodynamic characteristics for the bodies with grid fins in supersonic speeds.
介绍了超音速下格栅翼组合体的气动特性实验研究情况。 - This paper studies the effect of vectoring jet on the transverse aerodynamic characteristics of a slender body.
采用测压方法研究了矢量喷流对细长旋成体大迎角非对称流动的影响特性。 - The contradiction between bracing rigidity and aerodynamic interference can be resolved by this system.
该系统能解决支架的支撑刚度与气动干扰之间的矛盾。 - Aerodynamic force, moments, and longitudinal stability derivatives are estimated by three-dimensional low-order panel method.
涉及的气动力、力距和纵向稳定导数等则由三维低阶板块法计算获得。 - This paper introduces a wind tunnel experiment technique of side-back jet, aerodynamic interactions and predict method.
主要阐述了弹丸头部喷流风洞实验中的实验方法、动力干扰影响及预测方法。 - The ice accretion geometric characteristics have complex effects on airfoil aerodynamic coefficients.
积冰几何形状对翼型气动系数的影响是复杂的。 - The aerodynamic characteristics of airfoil are significantly influenced by non-equilibrium condensation of moist air.
湿空气非平衡凝结会对机翼的气动特性造成显著影响。 - The feasibility of counterflow scheme is validated by research on the internal aerodynamic characteristics of nozzle using numerical simulation.
利用数值模拟的方法,通过对逆流方案中喷管气动性能的研究验证了逆流推力矢量方案的可行性。 - This thesis presents the empirical method for prediction the aerodynamic coefficients on glide bullet.
本文主要对滑翔增程弹气动力工程计算进行了研究。