MHD slipstream accelerator investigation in the RPI hypersonic shock tunnel-Reference-Cited by-同舟云学术

MHD slipstream accelerator investigation in the RPI hypersonic shock tunnel

Published:1999-06-20 Issue: Volume: Page:
ISSN:
Container-title:35th Joint Propulsion Conference and Exhibit
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Author:

Kerl J.¹,Myrabo L.¹,Nagamatsu H.¹,Minucci M.¹,Meloney E.¹

Affiliation:

1. Rensselaer Polytechnic Inst., Troy, NY

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2842

Reference10 articles.

1. Static tests of jet fuel thermal and oxidative stability

2. Messitt, DG, "Computational and Experimental Investigation of 2-D Scramjet Inlets and Hypersonic Flow Over a Sharp Flat Plate" PhD Thesis Dissertation,Rensselaer Polytechnic Institute, Troy, NY,May, 1999.

3. Diaz, E, Toro, PGP, Myrabo, LN, Nagamatsu, HT, and Mess& DG, "Experimental Pressure Survey of the Hypersonic Air'Spike Inlet at Mach 10, "AIAA 96-3143, June 1996.

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