• 基本释义

  • 词形变化

1.NONLINEAR SUPERSONIC POTENTIAL FLOW OVER SIDESLIP CONICAL BODIES DELTA WINGS AND FUSELAGES
侧滑锥体、三维机翼与机身的超音速非线性全位势流计算收藏指正
2.Numerical Calculation of Aerodynamic Force Coefficient and Dynamic Stability Derivatives on Unsteady Supersonic Wing with Sideslip Angles
非定常超音速侧滑机翼的气动力系数及动导数的数值计算收藏指正
3.②height H=11000m, Mach number M=1.4, attack angle α = 10deg, sideslip angle β=0;
②高度11000米,马赫数为1.4,10度攻角;收藏指正
4.③height H=11000m, Mach number M=1.4, attack angle α=0, sideslip angleβ = 10 deg.
③高度11000米,马赫数为1.4,10侧滑角。收藏指正
5.Lifting Surface Theory and the Numerical Method of Wings with Small Angles of Sideslip at Subsonic and Supersonic Speeds
亚、超音速小侧滑角机翼升力面理论和数值计算方法收藏指正
6.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。收藏指正
7.The SHM (single hole microblowing) as a new perturbation active control technique has been applied to the slender body with different model noses at zero sideslip and high angle of attack.
摘要在亚临界流动范围内,对具有不同头部形状的尖拱形细长旋成体在无侧滑大迎角下进行单孔位微吹气扰动控制实验。收藏指正
8.Abstract: With the composite process of root-pile and infilling consolidation by cement injection with foraminate-steel-tube;Good effect has been made in the treat of sideslip of one fly-over bridge.The work machanism and technology of cement injection with foraminate-steel-tube are discussed in following article.
文摘:用树根桩及带眼钢管充填压密灌浆工艺复合处理某立交桥侧移的实践取得很好实效;对带眼钢管灌浆的工艺与机理作了讨论,认为其具有广阔的应用前景。收藏指正
9.The analysing results show that additive pullforce and sideforce moments are caused by aircraft PACTB in high angle of attack or high sideslip angle ,and these moments will cause the obvious effect for aircraft pitch and direction balance and bring unfavourable influence for pilot,controlling.
分析结果表明,飞机在大迎角或侧滑角下飞行时,螺旋桨气流斜吹使飞机产生了附加的拉力力矩和侧力力矩,对飞机俯仰和方向平衡有明显影响,给飞行员的操纵带来不利影响。收藏指正
10.A new type of actuate mechanism for the active reflector of FAST(five-hundredmeter aperture spherical telescope) radio telescope was proposed so that one can overcome the deficiency of original actuate mechanism. The mechanism was utilized to prevent from the sideslip in the margin cell of the active reflector,and to promote the mechanical efficiency and reliability,and to reduce the cost of manufacture and operate.
针对现有的FAST(Five-hundred-meter Aperture Spherical Telescope)主动反射面调整运动机构和促动器试验方案的不足,提出一种新型机构,能够有效地解决反射面边缘单元侧滑问题,并提高整个系统机械效率、可靠性,降低制造成本和运行维护费用.收藏指正
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