Development of Planar Doppler Velocimetry for Aircraft Exhausts

Author:

Jenkins Tom1,George Jacob1

Affiliation:

1. MetroLaser, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Reference15 articles.

1. where λLis the laser wavelength, a^ is a unit vector in the direction of observation, l^ is a unitvector in the direction of the laser, and Vr is the velocity vector of the fluid element being measured. The vectors are shown in Figure 7. The vector l a ^ ^ - represents the direction of the measured velocity component for the Doppler measurements presented here. It can be shown that fromthis geometrythe magnitude of the vector l a ^ ^ - isequalto 0.7654. Substituting this value into Eq. (1), and using 532 nm for the laser wavelength, the Doppler shift is computed to be -1.33 MHz per m/s. Figure 6. Configuration usedPDVexperiments in aturbojet engine

2. (m/s) 45K 100 -133 -115 86 55K 128 -170 -160 120 65K 160 -213 -230 172 74K 190 -253 -310 233 C. Doppler Shifts Measured in the Engine Exhaust

3. This work was supported by the Naval Air Warfare Center, Aircraft Division, under contract N68335-11-C0435.

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Planar Doppler Velocimetry in a Full-Scale Aircraft Engine Exhaust;AIAA SCITECH 2023 Forum;2023-01-19

2. Three-Component Velocity Measurements in a Turbine Engine Exhaust;55th AIAA Aerospace Sciences Meeting;2017-01-05

3. Three-Component Unseeded Velocity Diagnostic for Jet Engine Exhaust Flows;54th AIAA Aerospace Sciences Meeting;2016-01-02

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