afterburner 中文意思是什麼

afterburner 解釋
【航空】補燃器，加力燃燒室。

  1. Many jets have an afterburner.

    許多噴氣機都有加力燃燒室。
  2. Afterburner systems, designed to operate up to a stoichiometric overall mixture strength, are always fairly close to combustion instability or screech.

    要使加力燃燒系統在理論化學組成量的總混合濃度下還在一直工作，這樣的設計通常都很接近於不穩定燃燒或振蕩燃燒。
  3. Mouse control direction, the space bar afterburner

    鼠標控制方向，空格鍵加力。
  4. [ pilot ] initiating afterburner

    啟動后燃系統
  5. Pilot initiating afterburner

    啟動后燃系統
  6. Afterburner combustion system

    后燃燒系統
  7. This airplane can go out to high subsonic speeds very easily without using afterburner

    這架飛機能夠很輕松地在不打開加力的狀態下飛到高亞音速。
  8. Midway, it seemed that he had turned on an afterburner to roar across the finish line way ahead

    約翰遜跑到一半時突然爆發出驚人的力量沖過終點線。
  9. Because thermal insulation was in oxygen - riched condition of afterburner and charred layer was porous, oxygenous gas in mixture would penetrate into charred layer and chemical reaction would take place in whole charred layer, which intensified the ablation process

    由於絕熱層處於二次燃燒室富氧的環境中，而且炭化層為疏鬆多孔狀物質，因此將化學反應引入到整個炭化層中。
  10. Numerical simulation of two - phase turbulent combusti on flow in an afterburner under generalized nonorthogonal curvilinear coordinate systems

    非正交曲線坐標系數值模擬加力燃燒室湍流兩相流燃燒
  11. The combat radius range to 1, 100 km. with drop tanks the range can extend to 1, 300 kilometers. afterburner system is runing very smoothly. resonance is relatively smaller, compared with f16a / b

    作戰半徑可以達到1100公里。加掛副油箱可以延伸至1300公里。后燃加力系統運行平緩。共振比f - 16相對小一些。
  12. During the study of solid rocket ramjet ( srr ), ablation of afterburner thermal insulation is a serious problem, which cannot be ignored

    固沖發動機補燃室絕熱層的燒蝕問題是目前固沖發動機研製過程中所面臨的一個重要問題。
  13. In arbitrary curvilinear coordinates, the wall function is used for treating near wall regions. the influences of two different inlet gas parameter distributions and turbulent combustion models, as well as three different afterburners on turbulent combustion flow fields and wall temperature profiles are calculated. comparisons of experiment results and calculations results show that second - moment combustion model is reasonable for modeling turbulent reacting flows, inlet gas parameter distributions is more important. calculation method is reliable and can be used for the optimum design of afterburner

    數值研究三種不同幾何形狀、兩種進口氣流參數分佈、兩種紊流燃燒模型等對加力室內各氣流參數、隔熱屏和加力室筒體壁面溫度分佈的影響，計算結果與試驗數據比較表明:不同幾何形狀加力室對加力室內紊流燃燒流場的影響要比進口氣流參數分佈大些，正確給定進口氣流參數分佈較為重要，二階矩紊流燃燒模型更適用摸擬三維紊流燃燒流動，計算方法合理，編制的計算程序可靠，可供加力燃燒室優化設計用。
  14. In arbitrary curvilinear coordinate systems, three dimensional turbulent combustion flow fields of the three kinds of turbofan engine afterburner with the longitudinal heat shield 、 outer cold flow and the jet nozzle are simulated. the three - dimensional body - fitted grids are generated by an elliptical grid generation procedure and zone method

    本文在任意曲線坐標系統下對三種帶有縱向隔熱屏、外冷卻通道和尾噴管的渦扇發動機加力燃燒室的三維紊流燃燒流場進行數值模擬。
  15. An experiment system simulated afterburner oxygen - riched condition was established. the system was composed of ablation test motor, gas supply pipeline and measurement and control system

    該系統由富氧燒蝕發動機、氣路系統和測控系統組成，能夠模擬固沖發動機二次燃燒室富氧環境，進行絕熱層材料燒蝕試驗。
  16. Under the two - dimensional body - fitted coordinate, large - eddy simulation ( les ) of turbulent chemically reacting flows in the model afterburner with the v - gutter flame holder was carried out by using parallel computing

    本文在二維貼體坐標系下，對一帶v型穩定器的模型加力燃燒室燃燒流場採用大渦模型進行了并行數值模擬。
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