Chinese translation for "总压恢复系数"
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- stagnation pressure recovery factor
Related Translations:
恢复系: restorer linerestoring line 恢复系统: recovery systemrestoration system 恢复系数: coefficient of restitutioncollision coefficientrecovery coefficientrecovery factorreset raterestitution coefficient 弹性恢复系数: coefficient of elastic recovery 声音恢复系统: srs sound retrieval system 可恢复系数: restorable systemrestorablesystem 温度恢复系数: temperature recovery factortemperature-recovery factor
- Example Sentences:
| 1. | When there are struts at the divergent parts of inlet , the total pressure recovery coefficients and the kinetic energy coefficients of inlet decrease , and the flow distortion index increases obviously
当进气道扩压段有侧向支柱存在时，进气道总压恢复系数和动能系数均有所降低，而流场畸变指数则显著增大。 | | 2. | Experimental results of the air pumping of a serpentine inlet under ground running show that the total pressure recovery at the exit is low and the distortion at the exit is large
摘要对一种蛇形进气道开展了地面工作状态下的抽吸试验研究，结果表明，在该状态下进气道出口截面的总压恢复系数较低、流场畸变较大。 | | 3. | When the serpentine inlet is running at the exit mach number ma ( subscript e ) = 0 . 45 , the total pressure recovery coefficient equals 0 . 90 , and synthesis distortion equals 13 . 85 %
本研究的蛇形进气道在出口马赫数为0 . 45时，总压恢复系数为0 . 90 ，综合畸变指数为13 . 85 % ，总压恢复较低，畸变较大，超出了一般航空发动机的承受范围。 | | 4. | 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。 | | 5. | The results prove that : ( 1 ) when the mach number of the flow at the exit increases , the total pressure recovery decreases , and the circular steady total pressure distortion coefficient , turbulence intensity and synthesis distortion increase
研究结果表明： ( 1 )地面工作状态下，随着出口马赫数的增加，蛇形进气道出口截面的总压恢复系数不断下降，而稳态周向畸变指数、紊流度和综合畸变指数均上升，稳态径向畸变指数变化不大。 | | 6. | On the basis of these results , the relations of total - pressure recovery coefficient or flow coefficient and flight mach number , angle of attack and the second movable wedge angle of the inlet have been founded by hypersurface fitting , then the mathematical model of the inlet is established
根据流场计算结果并利用超曲面拟合方法建立了进气道总压恢复系数、流量系数与飞行马赫数、进气道攻角及二级可调斜板角度之间的关系，由此得到了二元混压式超声速进气道数学模型。 |
- Similar Words：
- "总压法" Chinese translation, "总压管" Chinese translation, "总压管理论" Chinese translation, "总压和静压差" Chinese translation, "总压恢复" Chinese translation, "总压降" Chinese translation, "总压孔" Chinese translation, "总压力" Chinese translation, "总压力80" Chinese translation, "总压力比" Chinese translation
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