LIGS measurements in the nozzle reservoir of a free-piston shock tunnel
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
http://link.springer.com/article/10.1007/s00193-018-0808-2/fulltext.html
Reference34 articles.
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2. Stalker, R.J., Paull, A., Mee, D.J., Morgan, R.G., Jacobs, P.A.: Scramjets and shock tunnels–the Queensland experience. Prog. Aerosp. Sci. 41(6), 471–513 (2005). https://doi.org/10.1016/j.paerosci.2005.08.002
3. Sander, T., Altenhöfer, P., Mundt, C.: Development of laser-induced grating spectroscopy for application in shock tunnels. J. Thermophys. Heat Transf. 28(1), 27–31 (2014). https://doi.org/10.2514/1.t4131
4. Sander, T., Altenhöfer, P., Mundt, C.: Temperature measurements in a shock tube using laser-induced grating spectroscopy. J. Thermophys. Heat Transf. 30(1), 62–66 (2016). https://doi.org/10.2514/1.t4556
5. Pearse, R., Gaydon, A.: The Identification of Molecular Spectra, 4th edn. Chapman and Hall, London (1976)
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1. Temperature and Velocity Measurement in a Shock Tube with Homodyne and Heterodyne Grating Spectroscopy;AIAA AVIATION 2023 Forum;2023-06-08
2. Simultaneous thermometry and velocimetry for a shock tunnel using homodyne and heterodyne detection;Applied Physics B;2022-07-23
3. In situ nozzle reservoir thermometry by laser-induced grating spectroscopy in the HELM free-piston reflected shock tunnel;Shock Waves;2021-01-09
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