Experimental and Numerical Investigation of a Solid-Fuel Rocket Scramjet Combustor-Reference-Cited by-同舟云学术

Experimental and Numerical Investigation of a Solid-Fuel Rocket Scramjet Combustor

Published:2016-03 Issue:2 Volume:32 Page:273-278
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Lv Zhong¹,Xia Zhi-xun¹,Liu Bing¹,Liu Yuan-chun¹

Affiliation:

1. National University of Defense Technology, 410073 Changsha, People’s Republic of China

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.B35838

Reference15 articles.

1. Hypersonic Airbreathing Propulsion

2. CurranE. T.MurthyS. N. B., Scramjet Propulsion, Vol. 31, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2000, pp. 369–439.

3. A Century of Ramjet Propulsion Technology Evolution

4. Introduction

5. WittM. A. “Investigation into the Feasibility of Using Solid Fuel Ramjets for High Supersonic Low Hypersonic Tactical Missiles,” M.S. Thesis, Naval Postgraduate School, Monterey, CA, 1989.

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