" ɚ 2009-2013 ɝɝ. 2. ɧɟɨɛɵɱɧɨ, ɞɟɦɨɧɫɬɪɪɪɭɹ 21 ɚɬ. (ɩɪɨɟɤɬ .
Экспериментальный стенд для исследования аэродинамики в вихревой топке нового типа
Схема вихревой топки нового типа
Ɋɟɡɭɥɶɬɚɬɵ ɬɟɨɪɟɬɢɱɟɫɤɢɯ ɢɫɫɥɟɞɨɜɚɧɢɣ ɩɨɤɚɡɚɥɢ, ɱɬɨ ɜ ɨɛɥɚɫɬɢ ɦɚ ɥɵɯ ɱɢɫɟɥ Ɋɟɣɧɨɥɶɞɫɚ (Re<1) ɩɪɢ ɤɪɢɬɢɱɟɫɤɨɦ ɡɧɚɱɟɧɢɢ ɱɢɫɥɚ Ȼɨɧɞɚ, ɪɚɜɧɨ ɦ ȼɨɤɪ=90, ɧɚɛɥɸɞɚɟɬɫɹ ɩɨɬɟɪɹ ɭɫɬɨɣɱɢɜɨɫɬɢ ɮɨɪɦɵ ɤɚɩɥɢ. Ⱦɥɹ ɷɤɫɩɟɪɢɦɟɧɬɚɥɶɧɨɝɨ ɢɫɫɥɟɞɨɜɚɧɢɹ ɩɨɬɟɪɢ ɭɫɬɨɣɱɢɜɨɫɬɢ ɮɨɪɦɵ ɱ ɚɫɬɢɰɵ ɞɢɫɩɟɪɫɧɨɣ ɮɚɡ ɩɪɢ ɦɚɥɵɯ ɱɢɫɥɚɯ Ɋɟɣɧɨɥɶɞɫɚ ɪɚɡɪɚɛɨɬɚɧɨ ɢ ɡɚ ɩɚɬɟɧɬɨɜɚɧɨ ɭɫɬɪɨɣɫɬɜɨ [1], ɩɨɞɪɨɛɧɨɟ ɨɩɢɫɚɧɢɟ ɤɨɬɨɪɨɣ ɩɪɢɜɟɞɟɧɨ ɜ ɪ ɚɛɨɬɟ [2]. Ⱦɥɹ ɭɱɟɬɚ ɜɧɭɬɪɟɧɧɟɝɨ ɬɟɱɟɧɢɹ ɠɢɞɤɨɫɬɢ ɜ ɤɚɩɥɟ ɩɪɢ Re<1 ɜ ɤɨɷɮɮɢɰɢɟɧ ɬ ɫɨɩɪɨɬɢɜɥɟɧɢɹ ɜɜɨɞɢɥɚɫɶ ɩɨɩɪɚɜɤɚ, ɩɨɥɭɱɟɧɧɚɹ ɢɡ ɪɟɲɟɧɢɹ Ɋɵɛɱɢɧɫɤ ɨɝɨ-Ⱥɞɚɦɚɪɚ ɞɥɹ ɡɚɞɚɱɢ ɜɹɡɤɨɝɨ ɨɛɬɟɤɚɧɢɹ ɫɮɟɪɢɱɟɫɤɨɣ ɤɚɩɥɢ.
U DH - ɩɨɬɟɧɰɢɚɥɶɧɚɹ ɷɧɟɪɝɢɹ ɨɬɞɟɥɶɧɨɣ ɦɨɥɟɤɭɥɵ ɝɚɡɚ, ɨɛɥɚɞɚɸɳɟɝɨ ɩɚɪ ɚ- ɢɥɢ ɞɢɚɦɚɝɧɢɬɧɵɦɢ ɫɜɨɣɫɬɜɚɦɢ, ɧɚɯɨɞɹɳɟɝɨɫɹ ɜɨ ɜɧɟɲɧɟɦ ɧɟɨɞɧɨɪɨɞ ɧɨɦ ɦɚɝɧɢɬɧɨɦ ɩɨɥɟ. -6 ɦ3) ɢ ɨɫɬɚɥɶɧɵɯ ɚɬɦɨɫɮɟɪɧɵɯ ɝɚɡɨɜ, ɨɛɥɚɞɚɸɳɢɯ ɞɢɚɦɚɝɧɢɬɧɵɦɢ ɫɜɨɣ ɫɬɜɚɦɢ, ɦɚɝɧɢɬɧɚɹ ɩɨɥɹɪɢɡɭɟɦɨɫɬɶ ɨɬɞɟɥɶɧɨɣ ɦɨɥɟɤɭɥɵ D - ɨɬɪɢɰɚɬɟɥɶɧɚ , ɬɨ ɩɥɨɬɧɨɫɬɶ ɤɢɫɥɨɪɨɞɚ ɜ ɫɦɟɫɢ ɝɚɡɨɜ ɛɭɞɟɬ ɭɜɟɥɢɱɢɜɚɬɶɫɹ ɜ ɨɛɥɚɫɬ ɢ ɫɢɥɶɧɨɝɨ ɦɚɝɧɢɬɧɨɝɨ ɩɨɥɹ, ɚ ɩɥɨɬɧɨɫɬɶ ɚɡɨɬɚ ɢ ɨɫɬɚɥɶɧɵɯ ɤɨɦɩɨɧɟɧ ɬ - ɭɦɟɧɶɲɚɬɶɫɹ, ɬ.ɤ. Ɉɞɧɚɤɨ ɬɟɱɟɧɢɟ ɀɆ ɜ ɦɚɝɧɢɬɧɨɦ ɩɨɥɟ (Ɇɉ), ɧɟɨɛɯɨɞɢɦɨɦ ɞɥɹ ɪɚɛɨɬɵ ɌəɊ ɬɢɩɚ ɌɈɄȺɆȺɄ, ɨɩɚɫɧɨ ɡɧɚɱɢɬɟɥɶɧɵɦ ɪɨɫɬɨɦ ɝɢɞɪɚɜɥɢɱɟɫɤɨɝɨ ɫɨɩɪɨɬɢɜ ɥɟɧɢɹ ɜ ɪɹɞɟ ɤɨɧɮɢɝɭɪɚɰɢɣ.
Ɋɚɫɫɦɚɬɪɢɜɚɟɦɚɹ ɤɨɧɮɢɝɭɪɚɰɢɹ ɬɟɱɟɧɢɹ ɢ ɨɛɨɝɪɟɜɚ
.
Ɉɫɪɟɞɧɟɧɧɨɟ ɩɨ ɩɟɪɢɦɟɬɪɭ ɱɢɫɥɨ ɇɭɫɫɟɥɶɬɚ ɜ ɡɚɜɢɫɢɦɨɫɬɢ ɨɬ ɧɟɨɞɧɨɪɨɞɧɨɫɬɢ ɨɛɨɝɪɟɜɚ
. Ɋɟɝɢɫɬɪɚɰɢɹ 11-ɢ .
Области решения задач
, [4].
TJ''cos
- Ɋɚɫɩɪɟɞɟɥɟɧɢɟ ɬɟɦɩɟɪɚɬɭɪ ɩɨ ɞɥɢɧɟ ɦɨɞɟɥɢ ɢɫɩɚɪɢɬɟɥɹ ɫ ɬɪɭɛɤɨɣ Ɏɢɥɶɞɚ
- Ȼɟɡɪɚɡɦɟɪɧɵɣ ɤɨɷɮɮɢɰɢɟɧɬ ɬɟɩɥɨɨɬɞɚɱɢ ɞɥɹ ɪɟɠɢɦɚ ɢɫɩɚɪɟɧɢɹ ɩɥɟɧɤɢ ɠɢɞɤɨɫɬɢ ɧɚ ɝɥɚɞɤɨɣ ɢ
- ɉɪɢɧɰɢɩɢɚɥɶɧɚɹ ɫɯɟɦɚ ɷɤɫɩɟɪɢɦɟɧɬɚɥɶɧɨɝɨ ɫɬɟɧɞɚ ɢɫɫɥɟɞɨɜɚɧɢɹ ɩɪɨɰɟɫɫɨɜ ɬɟɩɥɨɦɚɫɫɨɨɛɦɟɧɚ ɜ
- Визуализация вихревой дорожки с помощью поля завихренности, полученной методом PIV в
ɬɨɝɨ, , ɱɬɨ ɷɮɮɟɤɬ , ɜ . Ɋɚɛɨɬɚ «ɇɚɭɱɧɵɟ ɢ -ɩɟɞɚɝɨɝɢɱɟɫɤɢɟ ». .
Метод оптической фазовой триангуляции с расширенным динамическим диапазоном измерения
Исследование структуры закрученных потоков Дектерев Д.А
2.http://www.viessmann-moscow.ru/product/pumps/teplovoj _nasos_viessmann_vitocal_350 .. ɍȾɄ 532.62 XII Ɇɟɠɞɭɧɚɧɨɞɧɚɟ ɢɹ ɦɨɥɨɞɵɯ ɭɱɟɧɵɯ. Bakr et al, Determination of optical parameters of thin a-Si:H ¿lms deposited by hot wire - chemical vapor deposition technique using only transmission spectrum, Pramana - J. 1 ɚ) ɨɬɥɢɱɚɟɬɫɨ ɢɰ ɨɛɪɚɡɨɜɚɧɧɵɯ ɩɪɢ ɭɥɶɬɪɚɚɡɜɭɤɨɜɦɨ ɪɚɫɩɵɥɟɧɢɢ (ɪɢɫ. 2 ɛ), ɢ ɦɨɠɟɬ ɛɵɬɶ ɪɚɡɥɢɱɧɨɣ – ɫɩɥɨɲ- ɧɵɟ ɩɨɨɢɢɫɪɢɫɬɚɥɥɢɱɟɫɤɢɟ ɨɛɪɚ- ɡɨɜɚɧɢɹ, ɩɚɫɬɨɬɟɵɟ.
.
Ƚɟɨɦɟɬɪɢɱɟɫɤɚɹ ɨɛɥɚɫɬɶ ɬɟɱɟɧɢɹ
. ɬɨɝɨ, (1-10 ɧɦ) , ɡɚɜɢɫɹɳɭɸ , ɩɨɡɜɨɥɹɟɬ [1]. .
Ɂɚɞɚɱɟɣ ɞɚɧɧɨɣ ɪɚɛɨɬɵ ɛɵɥɨ ɩɪɨɜɟɞɟɧɢɟ ɬɟɫɬɨɜɵɯ ɢɡɦɟɪɟɧɢɣ ɦɟɬɨɞɨɦ PIV ɜ ɧɟɪɟɚɝɢɪɭɸɳɟɦ ɩɨɝɪɚɧɢɱɧɨɦ ɫɥɨɟ, ɜ ɩɨɝɪɚɧɢɱɧɨɦ ɫɥɨɟ ɫ ɝɨɪɟɧɢɟɦ ɢ ɫɨɩɨɫɬɚɜɥɟɧɢɟ ɪɟɡɭɥɶɬɚɬɨɜ ɢɡɦɟɪɟɧɢɣ ɫ ɞɚɧɧɵɦɢ ɱɢɫɥɟɧɧɨɝɨ ɦɨɞɟɥɢɪ ɨɜɚɧɢɹ. Ɋɟɲɚɥɚɫɶ ɡɚɞɚɱɚ ɜɡɚɢɦɨɞɟɣɫɬɜɢɹ ɞɜɭɦɟɪɧɵɯ ɚɤɭɫɬɢɱɟɫɤɢɯ ɜɨɥɧ ɫ ȼɍɋ ɧɚ ɩɥɚɫɬɢɧɟ ɫ ɜɫɬɚɜɤɨɣ ɢɡ ɬɪɭɛɱɚɬɵɯ ɤɚɧɚɥɨɜ ɫ ɩɪɹɦɵɦ ɡɚɞɚɧɢɟɦ ɝɟɨɦ ɟɬɪɢɢ ɤɚɧɚɥɨɜ ɜ ɪɚɫɱɺɬɧɨɣ ɨɛɥɚɫɬɢ (ɪɢɫ.1), ɬɚɤɠɟ ɤɚɤ ɜ [3]. ȼɵɩɨɥɧɟɧɨ ɩɚɪɚɦɟɬɪɢɱɟɫɤɨɟ ɢɫɫɥɟɞɨɜɚɧɢɟ ɜɥɢɹɧɢɹ ɪɚɡɦɟɪɚ ɩɨɪ, ɞɥɢɧ ɵ ɩɨɪɢɫɬɨɝɨ ɭɱɚɫɬɤɚ ɢ ɱɚɫɬɨɬɵ ɜɧɟɲɧɟɝɨ ɚɤɭɫɬɢɱɟɫɤɨɝɨ ɜɨɡɞɟɣɫɬɜɢɹ ɧɚ ɯɚɪɚɤɬɟɪɢɫɬɢɤɢ ȼɍɋ.
Ɂɚɜɢɫɢɦɨɫɬɶ ɬɟɦɩɟɪɚɬɭɪɵ ɨɬ ɜɪɟɦɟɧɢ Ȼɟɪɟɡɨɜɫɤɨɝɨ ɩɨɥɭɤɨɤɫɚ
Ɂɚɜɢɫɢɦɨɫɬɶ ɬɟɦɩɟɪɚɬɭɪɵ Ȼɟɪɟɡɨɜɫɤɨɝɨ ɩɨɥɭɤɨɤɫɚ ɨɬ ɜɪɟɦɟɧɢ
ⱦɥymedi ɖidi ɖidi ga aɖedi siadɨɨɨɨɨɬ ɢɥɨɨ ɥaɛ̃ ju . ɟmedi ɦɨɦɨɦɦɦ ŋutɔɤɤɤ ɪɥɥ ɭɨɨ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ ɩ dra . ɨɨ ɩɭɵɵɤ ɡɚ ɫɟɬ ɫɩɟɥɡɡ kurai ɡ kura . ɰɢɢ ɨɨɪmeɨɨɪ ɡɵicɤɤ. Ɂɞɟɫɶ ı, Ȥ, , ȡ, Ȝ, TS, – ɷɥɟɤɬɪɨɩɪɨɜɨɞɧɨɫɬɶ, ɬɟɩɥɨɩɪɨɨɨɬɬɬɧɨɨɨɬɬ ɦ drɔ̃e, drɔ̃e, drɔ̃e drɔ̃e, drɔ̃e drɔ̃e ɩɟɧɢɹ ɠɢɞɤɨɫɬɢ; ȝ – ɦɨɥɹɪɧɚɹ ɦɚɫɫɚ ɩɚɪɚ, Ⱥ – ɭɧɢɜɟɪɫɚɥɧɧɚɹ ɝɚɡɡɨɚɚɧɨɹɬ ɢɭɫ ɨɨɬɜɟɪɫɬɬɹ, U – ɧɚɩɪɹɠɟɧɢɟ ɧɚ ɷɥɟɤɬɪɞɨɚɯ, pa – ɞɚɠɨɨɢɟ ɫɤɧɨɟɱɧɫɬɢ. Ⱦɥɹ ɷɬɨɝɨ ɜ ɤɚɱɟɫɬɬɜɟ ɧɚɱɚɥɥɶɧɵɯ ɞɚɧɧɧɵɯ ɛɪɚɥɥɫɹ ɪɚɨɨɟɪɪɪɪɪɪɪɚ ɧɢɢɨɵ ɬɨ ɪɨɢɞɚɥɶɧɨɝɨ ɭɩɡɵɪɶɤɚ ɜ ɦɨɦɟɧɬ ɡɚɦɵɤɚɧɪɬɨɬɬɬɬɬɬɬɬɬɬ .
1. ɟɪɚɦɢ ɚ=0.025÷0.25mm ɜ ɡɚɜɢɫɢɦɨɫɬɢ ɨɬ ɧɚɩɪɹɠɟɧɢɹ ɧɚ ɷɥɟɤ (V) ). - ɪɵɦ ɝɢɞɪɚɜɥɢɱɟɫɤɢ ɩɨɞɨɛɧɵɦ ɦɨɞɟɥɶɧɵɦ ɩɨɪɢɦɩɬɤɨɛɧɵɦ ɦɨɞɟɥɶɧɵɦ ɩɨɪɢɦɩɬɦɦɪɢɨɦ ɦ ɤ ɧɢɠɧɟɣ ɫɬɟɧɤɟ ɤɚɧɚɥɚ. Ɍɚɤɢɦ ɨɛɪɚɡɨɦ, ɩɪɢ ɩɪɚɜɢɥɶɧɨɦ ɜɵɛɨɪɟ ɩɨɪɚɦɱɬ- ɪɨɢɜ ɢ ɫɤɚɹ ɩɨɫɬɚɧɨɜɤɚ (3)–(4) (1) -
Ɂɚɦɟɱɟɧɨ; ɩɨɫɨɛɨɦ, ɜɟɞɟɬ ɫɟɛɹ ɩɨ-ɪɚɡɧɨɦɭ, ɚ ɢɦɟɧɧɨ, ɜ ɛɨɥɶɲɨɨɟ ɫɹ ɜɪɟɦɹ ɩɪɨɫɚɱɢɜɚɧɢɹ ɠɢɞɤɨɫɬɢ ɜ ɨɛɪɚɡɟɰ (t=1÷10 ɦɢɧ).
Ʌɚɛɨɪɚɬɨɪɧɚɹ ɹɱɟɣɤɚ
Ɂɚɜɢɫɢɦɨɫɬɶ ɞɢɚɦɟɬɪɚ D ɤɚɩɥɢ ɨɬ ɜɪɟɦɟɧɢ t ɞɥɹ ɫɥɭɱɚɹ ɞɜɢɠɟɧɢɹ ɩɨ ɠɟɥɨɛɭ ɤɸɜɟɬɵ
Obtaining good visual scale of the flow structure in a wind tunnel has proven to be expensive and difficult. Visualization and imaging speed of particles in water reduces flow velocities due to Reynolds number characteristics. Detailed map of the velocity field near the tip vortices and the wake in general.
Water seeding was acceptable, with a slight tendency towards large particles. The design was flexible and allowed the freedom to move the model instead of the PIV equipment. The technique helped to establish an understanding of the conical vortices and flow in the inner channel, and also provided some wonderful videos and images for the report.
The average plots of full wake and visualization views were especially good at this. The relationship between blade tip speed ratio and expansion was confirmed. With PIV equipment, quantitative velocities were measured, indicating the sizes, structure, vorticity and eddy pairing of eddies.
The work was supported by the Ministry of Education and Science of the Russian Federation, grant ʋ.
Ɂɚɜɢɫɢɦɨɫɬɶ ɨɛɴɺɦɚ ɩɪɨɬɟɤɲɟɣ ɷɦɭɥɶɫɢɢ ɨɬ ɜɪɟɦɟɧɢ ɜ ɤɚɩɢɥɥɹɪɟ ɫ ɫɭɠɟɧɢɟɦ 43 ɦɤɦ ɩɪɢ
Исследование динамики жидкой газосодержащей оболочки в условиях невесомости Е.В. Резанова
- Зависимость изменения внутреннего радиуса оболочки со временем при различных исходных
- Ɂɚɜɢɫɢɦɨɫɬɶ ɬɟɦɩɟɪɚɬɭɪɵ ɧɚɬɪɢɹ ɧɚ ɜɵɯɨɞɟ ɢɡ ɚɤɬɢɜɧɨɣ ɡɨɧɵ ɨɬ ɜɪɟɦɟɧɢ ɜ ɫɬɚɰɢɨɧɚɪɧɨɦ ɪɟɠɢɦɟ
- Ɂɚɜɢɫɢɦɨɫɬɶ ɬɟɦɩɟɪɚɬɭɪɵ ɧɚɬɪɢɹ ɧɚ ɜɵɯɨɞɟ ɢɡ ɚɤɬɢɜɧɨɣ ɡɨɧɵ ɨɬ ɜɪɟɦɟɧɢ ɜ ɩɟɪɟɯɨɞɧɨɦ ɪɟɠɢɦɟ
- SEM ɦɢɤɪɨɮɨɬɨɝɪɚɮɢɹ ɩɨɜɟɪɯɧɨɫɬɢ ɮɨɥɶɝɢ
- ɋɪɚɜɧɟɧɢɟ ɪɚɫɱɟɬɚ ɫ ɨɩɵɬɧɵɦɢ ɞɚɧɧɵɦɢ [1], ɩɪɢ k = 0.35
Ɋɚɫɱɺɬɧɚɹ -600 ɷɥɟɦɟɧɬɵ: ɨɫɧɨɜɧɨɣ ɰɢɪɤɭɥɹɰɢɨɧɧɵɣ ; ;. -600 ɫɨɞɟɪɠɢɬ : ɬɟɩɥɨɨɛɦɟɧɧɢɤɢ ; ɝɥɚɜɧɵɟ ɰɢɪɤɭɥɹɰɢɨɧɧɵɟ ɧɚɫɨɫɵ (Ƚɐɇ-2);. 1 – ɬɟɦɩɟɪɚɬɭɪɵ - ; 2, 3 – ɬɟɦɩɟɪɚɬɭɪɵ (ɱɢɫɥɟɧɧɨɟ ɦɨɞɟɥɢɪɨɜɚɧɢɟ); 4 – ɫɤɨɪɨɫɬɢ (ɮɨɪɦɭɥɚ (1)); 5 – ɩɪɨɮɢɥɶ ɬɟɦɩɟɪɚɬɭɪɵ (5).
2. ɠɢɞɤɨɫɬɢ ɜ ɡɚɜɢɫɢɦɨɫɬɢ ɨɬ ɩɥɨɬɧɨɫɬɢ ɬɟɩɥɨɜɨɝɨ ɩɨɬɨɩ ɩɥɟɧɤɟ (Re=1300, ǻTɧɟɞ=70 °ɋ). i ɹ ɯ ɫɬɪɨɢɬɟɥɶɧɵɯ ɢɡɞɟɥɢɣ ɢ ɤɨɧɫɬɪɭɤɰɢɣ. ɏ ɡɨɜɚɧɢɢ ɦɟɬɨɞɚ ɦɚɥɨɭɝɥɨɜɨɝɨ ɪɚɫɫɟɹɧɢɹ, ɨɫɧɨɜɚɧɨɨɨɨɬ [ ɢ ɩɨ ɫɪɚɜɧɟɧɢɸ ɫ ɞɥɢɧɨɣ ɜɨɥɧɵ ɢɡɥɭɱɟɧɢɹ, ɩɨɞ ɦɚɥɵɤɢ ɭɭ ɜɥɟɧɢɸ ɩɚɞɚɸɳɟɝɨ ɢɡɥɭɱɟɧɢɹ.
. . (ɪɢɫ. 1, ɤɪɢɜɚɹ 2).
. ɢɰ ɩɨ ɪɚɡɦɟɟɪɚɦ.
Число Нуссельта, рассчитанное локально по длине обогреваемого канала. Поверхностное кипение
Два варианта расчетной области
Исследование теплообмена при плёночных течениях жидкости в условиях импульсного тепловыделения
Ɂɚɜɢɫɢɦɨɫɬɶ ɫɪɟɞɧɟɣ ɤɨɧɰɟɧɬɪɚɰɢɢ ɝɚɡɚ ɜ ɨɛɪɚɡɰɟ ɝɚɡɨɝɢɞɪɚɬɚ ɨɬ ɜɪɟɦɟɧɢ
Применение метода PIV для определения эффективности ингибирования метано - воздушного пламени добавкой аэрозоля K 4 [Fe(CN) 6 ]
Ɋɚɫɩɪɟɞɟɥɟɧɢɟ ɩɨɥɟɣ ɤɨɧɰɟɧɬɪɚɰɢɢ (ɨɛɴɟɦɧɵɟ ɞɨɥɢ) ɩɪɢ t=1000: a –ɦɨɞɢɮɢɰɢɪɨɜɚɧɧɵɣ ɬɢɩ ɡɚɝɪɭɡɤɢ 1; b
- , ɡɚɦɵɤɚɟɦɚɹ k H ɦɨɞɟɥɶɸ ɬɭɪɛɭɥɟɧɬɧɨɫɬɢ. - (ɤɪɨɦɟ ɞɢɦɟɪɨɜ) , ɭɫɬɨɣɱɢ- ɜɨɫɬɶ ɛɨɥɶɲɢɯ , , ɢɯ . Ɉɬɧɨɲɟɧɢɟ ɫɭɦɦɚɪɧɨɣ , CxHy+, ɤ Arn+ ɧɚ ɨɫɢ ɦɨɥɟɤɭɥɹɪɧɨɝɨ , ɦɦ ɱ.
Ʉɨɧɰɟɧɬɪɚɰɢɨɧɧɚɹ ɡɚɜɢɫɢɦɨɫɬɶ
, ɩɪɢɜɟɞɟɧɧɵɣ . . .
- , ɩɪɢɝɨɞɧɵɟ ɞɥɹ - , ɧɚ . Ɉɩɵɬɧɵɟ (ɪɢɫ.1) ɯɨɪɨɲɨ . .
Ʌɢɬɟɪɚɬɭɪɚ
[ ɝɚɡɨɜɵɯ ɤɥɚɫɬɟɪɨɜ ɞɥɹ ɨɛɪɚɛɨɬɤɢ ɩɨɜɟɪɯɧɨɫɬɧɵɯɢ ɨɪɵɯ ɯ ɫɥɨɺɜ ɦɚɬɟɪɢɚɥɚ. Ɋɚɡɥɢɱɚɸɬ ɬɪɢ ɨɫɧɨɜɧɵɯ ɬɢɩɚ ɦɨɞɢɮɢɤɚɰɢɢ ɦɚɬɟɪɢɚɥɤɧɧɨɬɚ ɵɦ ɩɨɬɨɤɨɦ: ɢɦɩɥɚɧɬɚɰɢɹ ɚɬɨɦɨɜ ɜ ɩɪɢɩɨɜɟɪɯɧɨɫɬɧɵɣ, [ ɟ ɬɨɧɤɢɯ ɩɥɺɧɨɤ. 2 (ɚ, ɛ) ɩɪɟɞɫɬɚɥɟɧɵ ɪɚɫɩɪɟɞɟɥɟɧɢɹ ɫɤɨɪɨɫɬɟɣɢ ɩɭɥɫɢɚɨɨɨ ɬ ɬɜɟ ɬɫɬɜɟɧɧɨ.
Ɋɚɫɱɟɬ ɫɨɫɬɚɜɚ ɫɢɫɬɟɦɵ, ɧɟɨɛɯɨɞɢɦɨɝɨ ɞɥɹ ɨɩɪɟɞɟɥɟɧɢɹ ɬɟɩɥɨɩɪɨɜɨɞɞ ɧɨɫɬɢ, ɩɪɨɜɨɞɢɥɫɹ ɩɪɢ ɩɨɦɨɳɢ ɩɪɨɝɪɚɦɦɵ ɌȿɌɊȺɇ, ɢɫɨɩɥɶɡɨ [2]. 2. ɝɥɹ ɫɪɟɞɧɟɝɨ ɫɨɫɬɚɜɚ, ɜɡɹɬɵɟ ɢɡ ɧɨɪɦɚɬɢɜɧɨɝɨ ɦɟɬɨɞɚ ɪɚɫɱɟɬɚ ɤɨɬ ɥɨɜ [5].
Micro-LIF, micro-LIF ɥɚ ɩɪɨɜɟɞɟɧɚ ɨɰɟɧɤɚ ɩɪɨɫɬɪɚɧɫɬɜɟɧɧɨɝɬɜɟɧɧɨɝɬɜɟɧɧɨɝɨɪɟɚ ɚ. 2. ɪɚ ɩɪɢ Re = 186 («ɡɚɯɜɚɬɵɜɚɸɳɢɣ ɪɟɠɢɦ»), ɩɨɥɭɱɟɧɧɵɟ ɫ ɩɨɦɫɩɷɤ LIF (ɫɩɪɚɜɚ) ɢ ɱɢɫɥɟɧɧɨɝɨ ɦɨɞɟɥɢɪɨɜɚɧɢɹ [2] (ɫɥɟɚɜɚ). Ɋɚɛɨɬɚ ɜɵɩɨɥɧɟɧɚ ɩɪɢ ɱɚɫɬɢɱɧɨɣ ɩɨɞɟɟɪɠɤɟ ɊɎɎɂ (ɝɪɚɧɧɣ ɩɨɞɟɪɠɤɟ ɎɊɎɂ ɧɬɚ ɈɉɌɗɄ ɞɥɹ ɦɨɥɨɞɵɯ ɢ Ɏɐɉ ɤɚɞɪɵ ɢɧɧɨɜɚɰɢɨɧɧɨɣ Ɋɨɫɫɢɢ».
1. ɪɚɡɨɜɚɧɢɟ ɭɞɚɪɧɨɣ ɜɨɥɧɵ. Ɋɟɡɭɥɶɬɚɬɵ ɞɚɸɬ ɜɨɡɦɨɠɧɨɫɬɶ ɨɩɪɟɞɟɥɢɬɶ ɩɪɟɞɟɥɶɧɨɬɬɭɬ ɰɢɢ ɩɪɢ ɡɚɞ ɚɧɵɯ ɨɫɬɚɥɶɧɵɯ ɜɢɛɪɚɰɢɢ ɪɢɚɥɚ, ɨɛɪɚɡɭɸɳɟɝɨ ɫɬɟɧɤɢ ɨɛɥɚɫɬɢ. Ɋɚɛɨɬɚ ɜɵɩɨɥɧɟɧɚ ɩɪɢ ɮɢɧɚɧɫɨɜɨɣ ɩɨɞɞɟɪɠɤɟ ɋɨɜɟɬɝɩɦɦɦ ɨɥ ɊɎ (ɇɒ.
Ⱦɚɧɧɵɣ (ɪɢɫ.1).
Ƚɟɨɦɟɬɪɢɹ ɢɫɫɥɟɞɭɟɦɵɯ ɦɨɞɟɥɟɣ
- Ɂɚɩɪɹɝɚɟɜ ȼ.ɂ., Ɇɢɪɨɧɨɜ ɋ.Ƚ ., Ɉɫɨɛɟɧɧɨɫɬɢ ɦɟɯɚɧɢɡɦɚ ɩɭɥɶɫɚɰɢɣ ɨɬɪɵɜɧɨɝɨ ɬɟɱɟɧɢɹ ɩɟɪɟɞ
- Ɂɚɩɪɹɝɚɟɜ ȼ.ɂ., Ʉɚɜɭɧ ɂ.ɇ., ɋɬɪɭɤɬɭɪɚ ɩɭɥɶɫɢɪɭɸɳɟɝɨ ɬɟɱɟɧɢɹ ɫ ɩɟɪɟɞɧɟɣ ɨɬɪɵɜɧɨɣ
DIL-402C ɨɢɡɜɨɞɫɬɜɚ ɮɢɪɦɵ NETZSCH (Ƚɟɪɦɚɧɢɹ) ɫ ɤɨɪɭɧɞɨɦɵɦɢɧɞɨɦɵɦɢ ɞɟɪɪ ɚɬɟɥɟ ɦ ɜ ɢɧɬɟɪɜɚɥɟ ɬɟɦɩɟɪɚɬɭɪ 293-1650 Ʉ ɨɨɢ ɫɚɝɪɟɜɟɟ 2 Ʉ/ɦɢɧ .
