Combustion Characteristics of the Solid-Fuel Ramjet with Star Solid Fuel-Reference-Cited by-同舟云学术

Combustion Characteristics of the Solid-Fuel Ramjet with Star Solid Fuel

Published:2018-07 Issue:4 Volume:31 Page:04018030
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Gong Lunkun¹,Chen Xiong²,Musa Omer³,Su Yingli⁴,Zhou Changsheng²

Affiliation:

1. Xi’an Modern Chemistry Research Institute, Xi’an 710065, China; formerly, School of Mechanical Engineering, Nanjing Univ. of Science and Technology, Nanjing 210094, China (corresponding author).

2. Professor, School of Mechanical Engineering, Nanjing Univ. of Science and Technology, Nanjing 210094, China.

3. School of Mechanical Engineering, Nanjing Univ. of Science and Technology, Nanjing 210094, China.

4. Master, School of Mechanical Engineering, Nanjing Univ. of Science and Technology, Nanjing 210094, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000839

Reference44 articles.

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2. Radius of Curvature Effects on Throat Thermochemical Erosion in Solid Rocket Motors

3. Brindle A. Boyce R. R. and Neely A. J. (2005). “CFD analysis of an ethylene-fueled intake-injection shock-induced-combustion scramjet configuration.” Proc. AIAA/CIRA 13th Int. Space Planes and Hypersonics Systems and Technologies AIAA Reston VA 2005–3239.

4. Scale effect of fuel regression rate in hybrid rocket motor

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