Prof. Omer Musa

College of Energy and Power Engineering

Nanjing University of Aeronautics and Astronautics, China

Associate Professor

Email: [email protected]; [email protected]

Qualifications

2017 Ph.D. in Aerospace Engineering, Nanjing University of Science and Technology, China

Publications (Selected)

1. Omer Musa*, Guoping Huang, Abdalazeem Adam, and Zonghan Yu. "Isolator shape transition impact on hypersonic internal waverider intake flow distortion." Physics of Fluids 36, no. 11 (2024).
2. Omer Musa*, Guoping Huang, and Zonghan Yu. "New third-order weighted essentially nonoscillatory scheme with novel compact nonlinear weights based on the forward-divided differences." Physics of Fluids 36, no. 9 (2024).
3. Omer Musa*, and Guoping Huang. "Improved design method for hypersonic intakes using pressure-corrected osculating axisymmetric flows method." AIAA Journal (2024): 63(1), 102-117.
4. Omer Musa*, and Guoping Huang. "New formulations for constructed polynomials and smoothness indicators of weighted essentially non-oscillatory schemes based on the forwarddivided differences." Physics of Fluids 36, no. 8 (2024).
5. Omer Musa, Guoping Huang, Zonghan Yu, Bo Jin*, Mohammad Javad Pour Razzaghi, “Startability analysis of hypersonic overboard spillage internal waverider intake based on new basic flowfield.” Physics of Fluids, 2024. 36(5).
6. Omer Musa*, Guoping Huang, Zonghan Yu. "Evaluation of the Pressure-Corrected Osculating Axisymmetric Flows Method for designing Hypersonic Wavecatcher Intakes with Shape Transition." Journal of Aerospace Engineering, 2024. 37(3): p. 04024023.
7. Omer Musa*, Guoping Huang, Bo Jin, Sannu Mölder, Zonghan Yu. "New Parent Flowfield for Streamline-Traced Intakes." AIAA Journal 61(7) (2023): 2906-2921.
8. Omer Musa*, G. Huang, and Z. Yu. "Assessment of new pressure-corrected design method for hypersonic internal waverider intake." Acta Astronautica 201 (2022): 230-246.
9. Omer Musa*, G. Huang, Z. Yu, Effects of new solid propellant configurations on the combustion characteristics of a ramjet, Aerospace science and technology, 119 (2021): 107192
10. Omer Musa*, G. Huang, M. Wang, A New Smoothness Indicator of Adaptive Order Weighted Essentially Non-Oscillatory Scheme for Hyperbolic Conservation Laws, Mathematics, 9(1) (2021) p. 69.
11. Omer Musa*, G. Huang, Z. Yu, Q. Li, An improved roe solver for high order reconstruction schemes, Computers & Fluids, 207 (2020) 104591.
12. Omer Musa*, Chen Xiong, Liao Wenhe, Weixuan Li, Combustion characteristics of a novel design of solid-fuel ramjet motor with swirl flow, Aerospace science and technology, 92 (2019): 750-765
13. Omer Musa, Chen Xiong, Li Yingkun, Liao Wenhe, Weixuan Li, Unsteady Simulation of Ignition of Turbulent Reactive Swirling Flow of Novel Design of Solid-Fuel Ramjet Motor, Energies, 2019, 12, 2513
14. Omer Musa*, Weixuan Li, Chen Xiong, Gong Lunkun, Liao Wenhe, "Experimental investigation on the effect of swirling flow on combustion characteristics and performance of solid fuel ramjet." Acta Astronautica, 2018.148: p. 163-174.
15. Omer Musa*, Chen Xiong, Zhou Changsheng, LiYingkun, LiaoWenhe, "Investigations on the influence of swirl intensity on solid-fuel ramjet engine." Computers & Fluids,167 (2018): 82-99.
16. Omer Musa*, Chen Xiong, Zhou Changsheng,Combustion characteristics and turbulence modeling of swirling reacting flow in solid fuel ramjet.Acta Astronautica, 2017.139: p. 1-17.
17. Omer Musa*, Chen Xiong, Zhou Changsheng, Experimental and numerical investigation on the ignition and combustionstability in solid fuel ramjet with swirling flow.Acta Astronautica, 2017. 137: p. 157–167.
18. Omer Musa*, Chen Xiong, Zhou Changsheng, Weixuan Li, Effect of inlet conditions on swirling turbulent reacting flows in a solid fuel ramjet engine.Applied Thermal Engineering, 2017. 113: p. 186-207.
19. Omer Musa*, Chen Xiong, Zhou Changsheng, Gong Lunkun, Assessment of the modified rotation/curvature correction SST turbulence model for simulating swirling reacting unsteady flows in a solid-fuel ramjet engine. Acta Astronautica, 2016. 129: p. 241–252.
20. Omer Musa, Zhou Changsheng, Chen Xiong*, Gong Lunkun, Prediction of swirling cold flow in a solid-fuel ramjet engine with a modified rotation/curvature correction SST turbulence model. Applied Thermal Engineering, 2016. 105: p. 737-754.

Profile Details

Web of Science ResearcherID: O-9384-2017

https://faculty.nuaa.edu.cn/OMERMUSAIBRAHIMMUSA/zh_CN/index.htm

https://orcid.org/0000-0003-3129-3902

https://scholar.google.com/citations?user=Awvf9DEAAAAJ&hl=en

www.researchgate.net/profile/Omer_Musa2