Feasibility study of a hybrid MHD/radiatively driven facility for hypersonic ground testing-Reference-Cited by-同舟云学术

Feasibility study of a hybrid MHD/radiatively driven facility for hypersonic ground testing

Published:1997-06-23 Issue: Volume: Page:
ISSN:
Container-title:28th Plasmadynamics and Lasers Conference
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Author:

Macheret Sergey¹,Miles Richard¹,Nelson Gordon²,Macheret Sergey¹,Miles Richard¹,Nelson Gordon²

Affiliation:

1. Princeton Univ., NJ

2. MSE, Inc., Butte, MT

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2429

Reference18 articles.

1. Radiatively driven hypersonic wind tunnel

2. S.Macheret, G.Williams, G.Comas, C.Meinrenken, W.Lempert, and R.Miles, "Energy Addition and Thermalization Issues inaRadiatively Driven HypersonicWind Tunnel", Paper AIAA 95-2142.

3. S.Macheret, C.Meinrenken, G.Williams, W.Gillespie, W.Lempert, and R.Miles, "Radiative Energy Addition to High Pressure SupersonicAir", Paper AIAA 96-1984.

4. G.L. Nelson and G. Simmons, "Augmentation of Hypersonic Propulsion Testing Facilities Using MHD", Paper AIAA 95-1937.

5. I.V.Adamovich, J.W.Rich, and G.L.Nelson, "Feasibility Study of MHDAcceleration of Unseeded and Seeded Air Flows", PaperAIAA 96-2347.

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