Development of a high‐frequency, second‐harmonic gyrotron tunable up to 636 GHz

1993 ◽  
Vol 5 (5) ◽  
pp. 1377-1379 ◽  
Author(s):  
T. Idehara ◽  
T. Tatsukawa ◽  
I. Ogawa ◽  
Y. Shimizu ◽  
S. Makino ◽  
...  
2017 ◽  
Vol 2017 (45) ◽  
pp. 83-89
Author(s):  
A.A. Marusenkov ◽  

Using dedicated high-frequency measuring system the distribution of the Barkhausen jumps intensity along a reversal magnetization cycle was investigated for low noise fluxgate sensors of various core shapes. It is shown that Barkhausen (reversal magnetization) noise intensity is strongly inhomogeneous during an excitation cycle. In the traditional second harmonic fluxgate magnetometers the signals are extracted in the frequency domain, as a result, some average value of reversal magnetization noises is contributed to the output signals. In order to fit better the noise shape and minimize its transfer to the magnetometer output the new approach for demodulating signals of these sensors is proposed. The new demodulating method is based on information extraction in the time domain taking into account the statistical properties of cyclic reversal magnetization noises. This approach yields considerable reduction of the fluxgate magnetometer noise in comparison with demodulation of the signal filtered at the second harmonic of the excitation frequency.


1991 ◽  
Vol 3 (7) ◽  
pp. 1766-1772 ◽  
Author(s):  
Toshitaka Idehara ◽  
Toshiaki Tatsukawa ◽  
Hidehiko Tanabe ◽  
Satoru Matsumoto ◽  
Kohji Kunieda ◽  
...  

2009 ◽  
Vol 4 ◽  
pp. 011-011 ◽  
Author(s):  
Takashi NOTAKE ◽  
Teruo SAITO ◽  
Yoshinori TATEMATSU ◽  
Akihito FUJII ◽  
Shinya OGASAWARA ◽  
...  

2020 ◽  
Author(s):  
Xiaotong Guan ◽  
Wenjie Fu ◽  
Jiayi Zhang ◽  
Dun Lu ◽  
Xiaolei Zheng ◽  
...  

2021 ◽  
pp. 1-1
Author(s):  
Mikhail Yu. Glyavin ◽  
Andrey N. Kuftin ◽  
Mikhail V. Morozkin ◽  
Mikhail D. Proyavin ◽  
Andrey P. Fokin ◽  
...  

2016 ◽  
Vol 2016 ◽  
pp. 1-14 ◽  
Author(s):  
Jianqiang Shi ◽  
Xiaojun Tang ◽  
Zhenqing Wang ◽  
Mingfang Shi ◽  
Wei Zhao

Direct numerical simulation (DNS) of a hypersonic compressible flow over a blunt wedge with fast acoustic disturbances in freestream is performed. The receptivity characteristics of boundary layer to freestream pulse acoustic disturbances are numerically investigated at Mach 6, and the frequency effects of freestream pulse wave on boundary layer receptivity are discussed. Results show that there are several main disturbance mode clusters in boundary layer under acoustic pulse wave, and the number of main disturbance clusters decreases along the streamwise. As disturbance wave propagates from upstream to downstream direction, the component of the modes below fundamental frequency decreases, and the component of the modes above second harmonic components increases quickly in general. There are competition and disturbance energy transfer between different boundary layer modes. The nose boundary layer is dominated by the nearby mode of fundamental frequency. The number of the main disturbance mode clusters decreases as the freestream disturbance frequency increases. The frequency range with larger growth narrows along the streamwise. In general, the amplitudes of both fundamental mode and harmonics become larger with the decreasing of freestream disturbance frequency. High frequency freestream disturbance accelerates the decay of disturbance wave in downstream boundary layer.


2020 ◽  
Vol 67 (3) ◽  
pp. 1234-1239
Author(s):  
Pengbo Wang ◽  
Xiaofeng Li ◽  
Junkai Liao ◽  
Xin Qi ◽  
Xiaotao Han ◽  
...  

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