Flow Speed Sensor Based on Optical Microresonators

AIAA Journal ◽  
2021 ◽  
pp. 1-8
Author(s):  
Elie R. Salameh ◽  
Alexandra K. Wise ◽  
Jaime da Silva ◽  
M. Volkan Ötügen ◽  
Dominique Fourguette
Optik ◽  
2020 ◽  
pp. 166118
Author(s):  
Zhen Li ◽  
Jiqiang Wang ◽  
Xiaoxing Zhong ◽  
Tongyu Liu ◽  
Yanong Ning ◽  
...  

Author(s):  
Toshio Nemoto ◽  
Yoshihiro Hashimoto ◽  
Sojun Sato ◽  
Hiroshi Iitaka

1997 ◽  
Vol 117 (7) ◽  
pp. 716-721
Author(s):  
Toshio Nemoto ◽  
Yoshihiro Hashimoto ◽  
Sojun Sato ◽  
Hiroshi Iitaka

2012 ◽  
Author(s):  
L. Rodriguez-Cobo ◽  
M. A. Quintela ◽  
M. Lomer ◽  
A. Cobo ◽  
J. M. Lopez-Higuera

1990 ◽  
Vol 160 (1) ◽  
pp. 157 ◽  
Author(s):  
Vladimir B. Braginskii ◽  
V.S. Il'chenko ◽  
M.L. Gorodetskii

1994 ◽  
Vol 13 (1) ◽  
pp. 59-65 ◽  
Author(s):  
Bernard Lefauconnier ◽  
Jon Ove Hagen ◽  
Jean Paul Rudant
Keyword(s):  

2017 ◽  
Vol 13 (3) ◽  
pp. 30-38
Author(s):  
Y. B. Gorbatkin ◽  
V. A. Chernyshev ◽  
S. S. Sevostyanov ◽  
A. V. Gladkov

The article is devoted to the development of a secondary converter for measuring the speed of turbo-pump aggregates of rocket engines. The principle of the induction speed sensor is considered in the article. A method is proposed for generating output pulses from signals of induction speed sensors, which consists in the preliminary integration of the signals of the speed sensor. This method allows to increase the reliability and accuracy of the formation of signals of induction speed sensors, as well as to increase the noise immunity of the secondary converter and significantly increase the dynamic range of measuring the speed. The data of flight tests of the developed secondary converter are given.


Sign in / Sign up

Export Citation Format

Share Document