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Experimental results of an investigation of two methods of inflight thrust measurement applicable to afterburning turbojet engines with ejectors

机译：两种飞行器推力测量方法研究的实验结果适用于带喷射器的加力涡轮喷气发动机

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作者
Bloomer, Harry E;
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年度 1958
页码 1-38
总页数 38
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Afterburning effect on the energetic and exergetic performance of an experimental turbojet engine (TJE) [J] . Ozgur Balli International Journal of Exergy . 2014,第2期

机译：加力对实验性涡轮喷气发动机（TJE）的能量和能量性能的影响
2. EXPERIMENTAL INVESTIGATION OF THRUST AUGMENTATION BY EJECTORS ON A PULSE DETONATION ENGINE [J] . Xi-Qiao Huang, Moqi Li, Zhuo Guo, Thermal science . 2015,第6期

机译：脉冲爆轰发动机射弹推力增强的实验研究
3. Experimental investigation of thrust augmentation by ejectors on a pulse detonation engine [J] . Huang Xi-Qiao, Li Moqi, Guo Zhuo, Thermal science . 2015,第6期

机译：脉冲爆震发动机上喷射器推力增强的实验研究
4. Prediction and Experimental Measurement of Total Temperature in an Afterburning Turbojet Exhaust [C] . Trevor M. Moeller, Robert Rhodes, Gregg R. Beitel, AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition . 2012

机译：加力涡轮喷气发动机排气中总温度的预测和实验测量
5. Study of ejector geometry on thrust augmentation for pulse detonation engine ejector systems. [D] . Shehadeh, Ra'fat. 2007

机译：脉冲爆震发动机喷射器系统推力增加时喷射器几何形状的研究。
6. Dataset of the experimentally measured heat transfer in the throat region of liquid rocket engine thrust chambers [O] . Marco Pizzarelli 2021

机译：实验测量的热传递的数据集在液体火箭发动机推力室的喉部区域中的热传递
7. 1 Experimental Investigation of Thrust Augmentation by Ejectors on a Pulse Detonation Engine [O] . Xi-qiao Huang, Moqi Li, Zhuo Guo, 2016

机译：1脉冲爆震发动机推力器推力增大的实验研究

Experimental results of an investigation of two methods of inflight thrust measurement applicable to afterburning turbojet engines with ejectors

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