Quantitative density measurement of wake region behind reentry capsule (Improvements in accuracy of 3D reconstruction by evaluating the view-angle of measurement system)-Reference-Cited by-同舟云学术

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Quantitative density measurement of wake region behind reentry capsule (Improvements in accuracy of 3D reconstruction by evaluating the view-angle of measurement system)

Published:2021 Issue:3 Volume:16 Page:JFST0021-JFST0021
ISSN:1880-5558
Container-title:Journal of Fluid Science and Technology
language:en
Short-container-title:JFST

Author:

YAMAGISHI Masato¹,YAHAGI Yusuke¹,OTA Masanori¹,HIROSE Yusuke²,UDAGAWA Shinsuke³,INAGE Tatsuro⁴,KUBOTA Shigeya⁵,FUJITA Koji⁶,OHTANI Kiyonobu⁶,NAGAI Hiroki⁶

Affiliation:

1. Graduate School of Engineering, Chiba University

2. Mechanical & Electronic Engineering, Tokyo Salesian College of Technology

3. Aerospace Engineering Course, Tokyo Metropolitan College of Industrial Technology

4. Department of Mechanical Engineering, Shonan Institute of Technology

5. Toyota Compact Car Company, TOYOTA Motor Corporation

6. Institute of Fluid Science, Tohoku University

Publisher

Japan Society of Mechanical Engineers

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering

Link

https://www.jstage.jst.go.jp/article/jfst/16/3/16_2021jfst0021/_pdf

Reference16 articles.

1. Carlson, Harry W. Correlation of sonic-boom theory with wind-tunnel and flight measurements. NASA Technical report, NASA TR R-213, (1964).

2. Nicolas, F., Todoroff, V., Plyer, A., Le Besnerais, G., Donjat, D., Micheli, F., Champagnat F., Cornic, P., Le Sant, Y., A direct approach for instantaneous 3D density field reconstruction from background-oriented schlieren (BOS) measurements, Experiments in Fluids, Vol. 57, No. 13 (2016)

3. Nicolas, F., Donjat, D., Micheli, F., Le Besnerais, G., Plyer, A., Cornic, P., Champagnat, F., Michou, Y., EXPERIMENTAL STUDY OF A COUNTER-FLOW JET IN ONERA’S S1MA WIND TUNNEL BY 3D BACKGROUND ORIENTED SCHLIEREN, 18^th ISFV, Zurich, Switzerland, (2018)

4. Joslin R. D. Aircraft laminar flow control. Annual review of fluid mechanics, Vol. 30 No. 1 (1998), pp1-29.

5. Gonzales, J., Kurihara, D., Nagai, H., Sakaue, H., Jemcov, A., Validation of Sub-millimeter resolution pressure measurement on free flight model mach 1.5, American Institute of Aeronautics and Astronautics (AIAA) SciTech Forum, (2021).

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1. Promotion of carbon dioxide adsorption using a zeolite-coated monolith with acoustic excitation;Journal of Fluid Science and Technology;2024

2. Formulation and demonstrations of three-dimensional background-oriented schlieren using a mirror for near-wall density measurements;Experiments in Fluids;2023-07

3. Estimating density, velocity, and pressure fields in supersonic flows using physics-informed BOS;Experiments in Fluids;2023-01

4. Background-oriented schlieren technique with vector tomography for measurement of axisymmetric pressure fields of laser-induced underwater shock waves;Experiments in Fluids;2022-11

5. Propagation Characteristics of Modulated EHF Signal in the Wake Region of Plasma Sheath;Aerospace;2022-04-04

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