TOP > Available Issues > Table of Contents > Abstract | | TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES |
| Vol. 45 (2002) , No. 150 p.217 |
| [PDF (351K)] [References] | | Application of a 20 kW Arc-Heated Wind Tunnel to Evaluation Tests of Wall Catalysis
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| | 1) Department of Aeronautics and Astronautics, Kyushu University 2) Takasago Research and Development Center, Mitsubishi Heavy Industries, Ltd. |
| (Received: October 12, 2001)
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| Abstract This paper describes the performance characteristics of a 20 kW-class arc-heated wind tunnel and the investigation of material catalysis as an application of this facility. First of all, stagnation heat fluxes and pressures are measured in high-enthalpy air and nitrogen arc jets that are generated by a constrictor-type arc heater. Total enthalpies of the arc jets are estimated based on Pope’s theory. The total enthalpies are 7.5–22 MJ/kg for nitrogen and 13–19 MJ/kg for air. The operation envelope of this arc-heated wind tunnel and the applicable conditions for reentry simulation or the thermal protection tests are discussed based on the experimental results. Finally, as an application of this arc-heated wind tunnel, evaluation tests of wall catalysis have been attempted by the use of two flat-faced cylindrical models equipped with two kinds of specimens of catalytic material. The evaluation tests are composed of heat flux measurements and spectroscopic measurements. It is found that there is a certain difference in obtained heat fluxes between the two catalytic materials. Emission spectra from a shock layer formed in front of the model are measured, and wall catalysis is discussed based on the spectra measurements. The results show the existence of catalytic wall effects. | | | | |  | To cite this article: |  | Makoto Hirakawa, Ken-ichi Abe, Michio Nishida, Ken-ichiro Takeishi and Masaaki Matsuura: “Application of a 20 kW Arc-Heated Wind Tunnel to Evaluation Tests of Wall Catalysis”, Trans. Japan Soc. Aero. S Sci., Vol. 45 (2003), pp.217-223 . |  |
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 | doi:10.2322/tjsass.45.217 |  | JOI JST.JSTAGE/tjsass/45.217 | | (c) 2005 The Japan Society for Aeronautical and Space Sciences |
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