nozzle area

基本解释

During the ground test under different working conditions of the gas generator, the influences of the radial clearance and exhaust nozzle area were studied.
根據發射系統內彈道計算模型，針對燃氣發生器噴喉麪積對導彈發射動力的影響進行導彈運動蓡數、內彈道性能的計算與分析。
In this part, calculation methods of the productivity, air-cushion pressure, air flow quantity, nozzle area, capacity of ventilator and electric motor are given out systematically.
系統給出了氣墊帶式輸送機生産率、氣墊壓力、空氣流量、氣孔麪積、鼓風機和電機功率的計算方法。
The model inputs include the fuel flow, the nozzle area, the altitude and Mach number, and model outputs include the rotor speed, the temperature and the air pressure.
模型的輸入量包括燃油流量、噴口麪積、高度及馬赫數，輸出量則包括高、低壓轉子的轉速及各截麪的溫度和壓力。