超临界翼的英文

• supercritical airfoil

• "超"英文翻译    exceed; surpass; overtake
• "临界"英文翻译    critical; crisis; criticalit ...
• "翼"英文翻译    the wing of a bird
• "超临界翼形" 英文翻译 :    airfoil; supercritical; supercritical airfoil
• "超临界翼技术" 英文翻译 :    supercritical wing
• "超临界翼型理论" 英文翻译 :    supercritical airfoil theory
• "超临界" 英文翻译 :    above-critical state; supercriticality
• "超临界抽提" 英文翻译 :    supercritical extraction
• "超临界的" 英文翻译 :    above critical; above-critical; hypercritical; overcritical; post stall; postcritical; supercritical
• "超临界电场" 英文翻译 :    overcritical electric field
• "超临界堆" 英文翻译 :    supercritical reactor
• "超临界范围" 英文翻译 :    supercritical range
• "超临界锅炉" 英文翻译 :    supercritical boiler
• "超临界氦" 英文翻译 :    supercritical helium
• "超临界回收" 英文翻译 :    supercritical recovery
• "超临界机翼" 英文翻译 :    supercritical wing; wing; supercritical
• "超临界机组" 英文翻译 :    supercritical unit
• "超临界角" 英文翻译 :    supercritical angle
• "超临界流" 英文翻译 :    hyper-critical flow; shooting flow; supercritical flow; supercritical stream; supercriticalflow
• "超临界流动" 英文翻译 :    supercritical flow
• "超临界流速" 英文翻译 :    higher critical velocity; velocity， supercritical
• "超临界流体" 英文翻译 :    supercritical fluid
• "超临界排气" 英文翻译 :    supercritical exhaust; supercritical gaseous discharge
• "超临界气流" 英文翻译 :    airflow; supercritical
• "超临界区域" 英文翻译 :    aupercritical range

• On comparing flutter characteristics of three supercritical airfoils in transonic flow
  超临界翼型的跨声速颤振特性研究
• Furthermore , numerical simulations for steady or unsteady transonic flow of rae2822 and dfvlr - r2 supercritical airfoils and a supercritical wings are investigated . the numerical results are in good agreement with experimental data where available
  进而，应用该解算器对超临界翼型rae2822 、 dfvlr - r2及某超临界机翼的定常或非定常流场进行了数值计算研究，得出了良好、合理的结论。
• The investigation in this dissertation shows the capabilities of ausm + scheme , such as the exact resolution of shock , low numerical dissipation , simple and requiring less computational effort . the successful applications on supercritical airfoils and wings show that the present flow solvers based on ausm + scheme are of valuable and promising in practical application
  通过本文的研究工作，展示了ausm +格式的激波高分辨率、数值耗散小、编程简洁、计算量较小等特性，同时，将其成功地应用于跨音速超临界翼型、机翼的定常或非定常气动特性的数值模拟和颤振研究中，具有一定的工程应用价值和良好的发展前景。