Chinese translation for "hypersonic flight"
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- 高超音速飞行
极音速飞行
Related Translations:
- Example Sentences:
| 1. | The calculations of aerodynamic heating and viscous friction forces on the surface of hypersonic flight vehicle
高超声速飞行器表面气动热和粘性摩擦力计算 | | 2. | Rocket - based combined cycle ( rbcc ) will be promising propulsion system to achieve hypersonic flight , and has extensively application foreground in both military and civil usage
火箭基组合循环( rbcc )推进系统是实现高超声速飞行的最有潜力的动力方案，具有广泛的军事和民用航天应用前景，因而备受瞩目。 | | 3. | As a kind of new configuration waveriders have high lift to drag ratio ( l / d ) in hypersonic flight , which makes the study of waverider shapes an important trend of hypersonic air vehicles development
乘波构形在高超声速条件下的高升阻比优势备受关注，使得对于它的设计研究成为高超声速飞行器外形设计的一个重要方向。 | | 4. | ( 2 ) to evaluate the effects of a reaction control jet on the aerodynamic performance of a missile operating at supersonic / hypersonic flight condition , the single and two attitude jet - interaction flow between a lateral jet and the external flow has been analyzed by detailed numerical simulation
( 2 )分别计算了单喷流和双喷流干扰流场。详细分析了流场结构和弹体表面压力分布特性，获得了一些有实用价值的结果。 | | 5. | Scramjet inlet is of great importance in the hypersonic airbreathing propulsion system and plays significant role in the realization of hypersonic flight . full 3 - dimensinal n - s equations are solved by using finite volume method , second - order harten - tvd spatial scheme , and algebraic baldwin - lomax turbulence model
本文基于favre质量加权平均的三维navier - stokes方程,采用有限体积法、二阶的tvd格式进行流场求解,并使用了bladwin - lomax代数湍流模型。 | | 6. | In the condition of non - axisymmetrical stage separation in hypersonic flight , the problems of dynamics and kinematics of the validating vechicle and the launch vechicle are primarily analysised . it includes the movement of the center of mass and the rigid body of the vechicles , the relative movement of the different vechicles , the relative movement of the special parts of the different vechicles , the load analysis and the probable collision in the process of stage separation
研究了在高超声速状态下非对称级间分离过程中,验证飞行器与运载火箭分离时的相关运动学和动力学问题。包括:飞行体质心运动和刚体运动;不同飞行体之间的相对运动;不同飞行体上特殊部位之间的相对运动;分离过程中各相关飞行体上的载荷分析和分离过程中可能发生的碰撞问题。 |
- Similar Words：
- "hypersonic density ratio" Chinese translation, "hypersonic eed" Chinese translation, "hypersonic engine" Chinese translation, "hypersonic era" Chinese translation, "hypersonic facility" Chinese translation, "hypersonic flight environment simulator" Chinese translation, "hypersonic flow" Chinese translation, "hypersonic flow condition" Chinese translation, "hypersonic flutter" Chinese translation, "hypersonic forces" Chinese translation
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