Combustion Characteristics of Paraffin-Polyethylene Blends Fuel for Solid Fuel Ramjet

Author:

Li Weixuan1,Chen Xiong2ORCID,Su Yingli3,Musa Omer4

Affiliation:

1. Ph.D. Candidate, School of Mechanical Engineering, Nanjing Univ. of Science and Technology, Nanjing 210094, China.

2. Professor, School of Mechanical Engineering, Nanjing Univ. of Science and Technology, Nanjing 210094, China (corresponding author). ORCID: .

3. Engineer, COMAC Shanghai Aircraft Design and Research Institute, 5188 Jinke Rd., Shanghai 200000, China.

4. Postdoctoral Student, 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

Reference28 articles.

1. Cai W. 2002. “Two-phase flow interactions and combustion of AP/HTPB composite propellant in rocket motors with acoustic oscillations.” Ph.D. dissertation Dept. of Mechanical Engineering Pennsylvania State Univ.

2. Trade-off between paraffin-based and aluminium-loaded HTPB fuels to improve performance of hybrid rocket fed with N2O

3. De Wilde J. P. 1991. “Fuel pyrolysis effect on hybrid rocket and solid fuel ramjet combustor performance.” Ph.D. dissertation Dept. of the Aerodynamics Wind Energy Flight Performance and Propulsion Delft Univ. of Technology.

4. Fuel Regression Mechanism in a Solid Fuel Ramjet

5. Hoegl A. and D. Duesterhaus. 1988. “Measurement in a solid fuel ramjet combustion with swirl.” In Proc. 24th Joint Propulsion Conf. 3045. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1988-3045.

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