Computational Study of the Propulsive Characteristics of a Shcramjet Engine-Reference-Cited by-同舟云学术

Computational Study of the Propulsive Characteristics of a Shcramjet Engine

Published:2008-01 Issue:1 Volume:24 Page:34-44
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Alexander Derrick C.¹,Sislian Jean P.¹

Affiliation:

1. University of Toronto, Toronto, Ontario M3H 5T6, Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.29951

Reference38 articles.

1. Hypervelocity Fuel/Air Mixing in a Shcramjet Inlet

2. Numerical Simulation of a Real Shcramjet Flowfield

3. Review of Fuel Pre-injection Studies in a High Speed Airflow

4. Hypervelocity Fuel/Air Mixing in Mixed-Compression Inlets of Shcramjets

5. Alexander, D. C. "Hypersonic Mixed-Compression Inlet Shock-Induced Combustion Ramjets," Ph.D. Thesis, Graduate Dept. of Aerospace Science and Engineering,Univ. of Toronto, Toronto,2006.

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