Blowdown Arc Facility for Low-Density Hypersonic Wind-Tunnel Testing-Reference-Cited by-同舟云学术

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Blowdown Arc Facility for Low-Density Hypersonic Wind-Tunnel Testing

Published:2001-11 Issue:6 Volume:38 Page:946-948
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Zuppardi Gennaro¹,Esposito Antonio¹

Affiliation:

1. Universita` di Napoli “Federico II”, 80125 Naples, Italy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/2.3769

Reference11 articles.

1. Bird, R. B., Stewartson, W. E., and Lightfoot, E. N., Transport Phenomena, 1st ed., Ambrosiana,Milan, 1960, pp.518-523(inItalian).

2. Bird, G. A., Molecular Gas Dynamics and the Direct Simulation of Gas Flows, Clarendon, Oxford, 1998, pp.1-23, 40, 41.

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1. A Combustion-Driven Facility for Hypersonic Sustained Flight Simulation;Aerotecnica Missili & Spazio;2024-04-17

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3. Extension of the Frozen Sonic Flow Method to Mixtures of Polyatomic Gases;AIAA Journal;2020-01

4. Frozen Sonic Flow Method Applied to Arc-Heated Facilities for Planetary Re-Entry Simulation;Aerotecnica Missili & Spazio;2018-07

5. Aerodynamic characterization of the jet of an arc wind tunnel;AIP Conference Proceedings;2016

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