Fast temperature measurement by infra-red line scanning in a hypersonic shock tunnel

Author:

Henckels A.,Maurer F.,Olivier H.,Grönig H.

Publisher

Springer Science and Business Media LLC

Subject

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

Reference6 articles.

1. Allegre, J. A.; Heriard Dubreuilh, X. H.; Raffin, M. 1988: Measurement of aerodynamic heat rates by infrared thermographic technique at rarefied flow conditions. In: Rarefied gas dynamics: physical phenomena. Progress in Astronautics and Aeronautics (eds. Müntz, E. P.; Weaver, D. P.; Campbell, D. H.). Vol. 117, pp. 157–167. Washington 1989: AIAA

2. Bouchardy, A. M.; Durand, G.; Gauffre, G. 1983: Processing of the infrared thermal images for aerodynamic research. SPIE Int. Technol. Conf. Geneva, TP no. 1983-32, ONERA Chatillon

3. Boylan, D. E.; Carver, D. B.; Stallings, D. W.; Trimmer, L. L. 1978: Measurement and mapping of aerodynamic heating using a remote infrared scanning camera in continuous flow wind tunnels. AIAA Paper 78-799, 213–231

4. Henckels, A.; Maurer, F. 1989: Application of infra-red thermography in a hypersonic blowdown wind tunnel. In: ICIASF '89 Record. pp. 516–524. New York: IEEE Publication 89CH2762-3

5. Simeonides, G.; Van Lierde, P.; Van der Stichele, S.; Capriotti, D.; Wendt, J. F. 1989: Infrared thermography in blowdown and intermittent hypersonic facilities. AIAA Paper no. 89-0042

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