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1-6 of 6
Keywords: solid rocket motor
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Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Energy Resour. Technol. November 2024, 146(11): 112101.
Paper No: JERT-24-1317
Published Online: July 26, 2024
.... Email: amano@uwm.edu Contributed by the Advanced Energy Systems Division of ASME for publication in the J ournal of E nergy R esources T echnology . 15 05 2024 02 07 2024 03 07 2024 26 07 2024 Graphical Abstract Figure solid rocket motor multiphase...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Energy Resour. Technol. September 2023, 145(9): 092301.
Paper No: JERT-22-1729
Published Online: March 28, 2023
... the solid rocket motor nozzle. The two-phase flow field caused by the propellant combustion process was simulated using the Eulerian–Lagrangian approach. Model validation was conducted using experimental and numerical published data. Then, the model was used to study the effect of aluminum/aluminum oxide...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Energy Resour. Technol. August 2022, 144(8): 082305.
Paper No: JERT-21-1807
Published Online: December 8, 2021
...Mohamed Abousabae; Ryoichi S. Amano Investigating the mechanical erosion of the solid rocket motor convergent-divergent (C-D) nozzle is essential to overcome its development barriers. Consequently, the break-up mechanism of the aluminum oxide agglomerates was studied to determine the influence...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Energy Resour. Technol. May 2021, 143(5): 052108.
Paper No: JERT-20-2038
Published Online: January 27, 2021
...Mohamed Abousabae; Ryoichi S. Amano; Cody Casper This study aims to better understand the aluminum oxide agglomerates breakup mechanism, consequently determining the best solution for the solid rocket motor (SRM) nozzle erosion problem. Two-phase air-water flow experimental investigation...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Energy Resour. Technol. September 2020, 142(9): 091301.
Paper No: JERT-19-1697
Published Online: April 8, 2020
...Wei-Lin Chen; Ahmad I. Abbas; Ryan N. Ott; Ryoichi S. Amano Aluminized propellants are frequently used in solid rocket motors (SRMs) to increase specific impulse. However, as the propellant combusts, the aluminum is oxidized into aluminum oxide (Al 2 O 3 ), it agglomerates into molten droplets...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Energy Resour. Technol. May 2020, 142(5): 052102.
Paper No: JERT-19-1696
Published Online: February 12, 2020
...Wei-Lin Chen; Ahmad I. Abbas; Ryan N. Ott; Ryoichi S. Amano This paper presents a solid rocket motor (SRM), both experiment and simulation of alumina molten flow patterns using the cold flow case. The combustion of aluminum composite propellants in SRM chambers causes high-temperature and pressure...