Experimental investigation of a 2-D dual mode scramjet with hydrogenfuel at Mach 4-6-Reference-Cited by-同舟云学术

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Experimental investigation of a 2-D dual mode scramjet with hydrogenfuel at Mach 4-6

Published:1990-08-17 Issue: Volume: Page:
ISSN:
Container-title:2nd International Aerospace Planes Conference
language:
Short-container-title:

Author:

VINOGRADOV V.¹,GRACHEV V.¹,PETROV M.¹,SHIKHMAN IU.¹

Affiliation:

1. Tsentral'nyi Nauchno-Issledovatel'skii Institut Aviatsionnogo Motorostroeniia, Moscow, USSR

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1990-5269

Reference7 articles.

1. ratio 0 - M m= 6.2.1-11 rows.fl-Ym= i : I 1 rows, q - M m = 5. IV row. 0 -E.= < I \ ' row Fig.10 Combustion efficiency aiong rhe

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