双语例句
- In this paper, the calculational methods of air flow through the general aircraft nacelles are established according to the structure characteristic and bleeding-exhaust form.
本文通过分析飞机发动机短舱的结构特点和引排气形式,建立了飞机典型短舱冷气流量的计算方法。
权威例句
Simulated transonic flows for aircraft with nacelles, pylons, and wingletsA technique for the inverse aerodynamic design of nacelles and wing configurationsInverse Design Method for Designing Isolated and Wing-Mounted Engine NacellesDesigning and Testing a Blended Wing Body with Boundary-Layer Ingestion NacellesAn Inverse Design Method for Designing Isolated and Wing-Mounted Engine NacellesModifications to jet aircraft having aft fuselage-mounted nacelles overlapping the wing assembliesMulti-physics power hardware in the loop test bench for on-shore wind turbine nacellesDesign and Testing of a Blended Wing Body with Boundary Layer Ingestion Nacelles at High Reynolds Numbers (Invited)Evaluation of Alternative In-Flight Fire Suppressants for Full-Scale Testing in Simulated Aircraft Engine Nacelles and Dry Bays (NIS...Comparison of zero-lift drags determined by flight tests at transonic speeds of symmetrically mounted nacelles in various spanwise p...