Characterization of CO2 flow in a hypersonic impulse facility using DLAS

Author:

Meyers J. M.,Paris S.,Fletcher D. G.

Funder

Air Force Office of Scientific Research

Centre National d’Etudes Spatiales

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Reference30 articles.

1. Arroyo MP, Langlois S, Hanson RK (1994) Diode laser absorption technique for simultaneous measurements of multiple gas dynamic parameters in high speed flows containing water vapor. Appl Opt 33(15):3296–3307. doi: 10.1364/AO.33.003296

2. Backx E (1974) The total temperature in the longshot wind tunnel: its measurement and evaluation. In: Technical Note 98. von Kármán Institute for Fluid Dynamics, Rhode-Saint-Genese, Belgium

3. Charbonnier JM, Paris S, Dieudonn W (1997) Extensions of the operating domain of the VKI longshot tunnel to the use of testing gases with various $$\gamma$$ values. In: 87th supersonic tunnel association, Modane, France

4. Danehy PM, Alderfer DW, Inman JA, Berger KT, Buck GM, Schwartz RJ (2008) Fluorescence imaging and streamline visualization of hypersonic flow over rapid prototype Wind-Tunnel Models. Proc IMechE Part G J Aerosp Eng 222(G5):637–651. doi: 10.1243/09544100JAERO295

5. Fay JA, Riddell FR (1958) Theory of stagnation point heat transfer in dissociated air. J Aeronaut Sci 25(2):73. doi: 10.2514/8.7517

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