Numerical Study of a Supersonic Nozzle Gas Jet Laden with a Dry Powder Fire-extinguishing Agent Injected from a Bypass Injector.

Authors: Zhang, L.¹, langzichsh@zstu.edu.cn, Wu, S.¹, Feng, Y.¹, Guan, H.¹

Source: Journal of Applied Fluid Mechanics; Apr2025, Vol. 18 Issue 4, p1098-1114, 17p

Aerodynamic Performance of Different Trailing-edge Serrations for High Reynolds Number Flows around Wing-flap System.

Authors: Ahmadkhah, S.¹, Jahangirian, A.¹, ajahan@aut.ac.ir, Zarinvafa, A.¹

Source: Journal of Applied Fluid Mechanics; Apr2025, Vol. 18 Issue 4, p1035-1047, 13p

Performance Analysis of Grid Topologies and RANS Turbulence Models in Predicting Aerodynamic Drag Coefficient at Zero-yaw for an Artillery Projectile.

Authors: Ferfouri, A.¹, Jerković, D. D.¹, damir.jerkovic@va.mod.gov.rs, Hristov, N.¹, Kari, A. V.², Allouche, T.¹

Source: Journal of Applied Fluid Mechanics; Mar2025, Vol. 18 Issue 3, p585-600, 16p

Fuel Reactivity Controlled Autoignition and Combustion Characteristics in a Supersonic Combustor With Different Turbulence Models.

Authors: Wang, Zihan¹ (AUTHOR), Luo, Qi¹ (AUTHOR), Lv, Yifan¹ (AUTHOR), Liu, Zuming¹ (AUTHOR), Han, Ziang¹ (AUTHOR), Li, Xiaojie¹ (AUTHOR) lixiaojie@nbu.edu.cn, Liou, William W.¹ (AUTHOR) william.liou@wmich.edu

Source: International Journal of Aerospace Engineering. 2/12/2025, Vol. 2025, p1-15. 15p.

Subject Terms: *MACH number, *COMBUSTION efficiency, *HEAT of combustion, *SUPERSONIC flow, *METHANE as fuel

Large-Eddy Simulation of Droplet Deformation and Fragmentation Under Shock Wave Impact.

Authors: Rossano, Viola¹, viola.rossano@unicampania.it, De Stefano, Giuliano¹, giuliano.destefano@unicampania.it

Source: Applied Sciences (2076-3417); Feb2025, Vol. 15 Issue 3, p1233, 19p

Noise Reduction Using Synthetic Microjet Excitation in Supersonic Rectangular Jets.

Authors: Marques, Michael¹, golubd1b@erau.edugoncalvm@my.erau.edusinghs36@erau.edu, Singh, Surabhi¹, Lyrintzis, Anastasios¹, Golubev, Vladimir¹, goncalvm@my.erau.edu

Source: Applied Sciences (2076-3417); Feb2025, Vol. 15 Issue 3, p1180, 20p

Experimental Dynamic Stability Investigation on Orion Entry Capsule in Supersonic Flow.

Authors: Sargolzaie, M.¹, Fazeli, H.², fazeli@mut.ac.ir, Soltani, M. R.³

Source: Journal of Applied Fluid Mechanics; May2025, Vol. 18 Issue 5, p1301-1311, 11p

Control of flow deflection angle around the corner using microjet array.

Authors: Nakadori, Yuto¹ (AUTHOR), Yuura, Satoshi¹ (AUTHOR), Kagawa, Takahiro¹ (AUTHOR), Urita, Akira¹ (AUTHOR), Handa, Taro¹ (AUTHOR) handa@toyota-ti.ac.jp

Source: Scientific Reports. 1/6/2025, Vol. 14 Issue 1, p1-10. 10p.

Subject Terms: *PARTICLE image velocimetry, *MACH number, *FLOW velocity, *DATA reduction, *VERY light jets

A comparative study o 135 f turbulence models for predicting the aerodynamic drag of a spin-stabilized projectile.

Alternate Title: Un estudio comparativo de modelos de turbulencia para predecir la resistencia aerodinámica de un proyectil estabilizado por giro.
Сравнительное исследование моделей турбулентности для прогнозирования аэродинамического сопротивления снаряда стабилизируемого вращением.
Компаративна студија модела турбуленције за предвиђање аеродинамичког отпора код пројектила стабилизованог ротацијом око уздужне осе.

Authors: Nguyen, Quang Tuan¹ tuannguyenmta28@gmail.com

Source: Military Technical Courier / Vojnotehnicki Glasnik. Jan-Mar2025, Vol. 73 Issue 1, p115-135. 21p.

Subject Terms: *MACH number, *COMPUTATIONAL fluid dynamics, *SUPERSONIC flow, *DRAG (Aerodynamics), *AERODYNAMICS

Development of a computational framework for low-Reynolds number propeller aeroacoustics.

Authors: SZULC, O.¹ oskar.szulc@imp.gda.pl, SURESH, T.¹, FLASZYŃSKI, P.¹

Source: Archives of Mechanics. 2025, Vol. 77 Issue 1, p67-85. 19p.

Subject Terms: *COMPUTATIONAL fluid dynamics, *MACH number, *FLOW separation, *SOUND pressure, *BOUNDARY layer (Aerodynamics)

A Novel Approach for Aircraft Engine Modeling Considering the Energy Accumulation Effect Based on a Variable Mass System Thermodynamics Method.

Authors: Dong, Huazhao^1,2 (AUTHOR) dhz0127@nuaa.edu.cn, Lian, Wenlei^1,2 (AUTHOR) wenlian@nuaa.edu.cn

Source: Energies (19961073). Dec2024, Vol. 17 Issue 24, p6424. 13p.

Subject Terms: *MACH number, *TURBOJET engines, *SIMULATION methods & models, *DYNAMIC simulation, *AIRPLANE motors

Aeroelastic flutter analysis of tilted curved nanopipe in supersonic flow.

Authors: Wu, Ke¹ (AUTHOR), Wang, Gang¹ (AUTHOR) 18515831495@163.com, Li, Xin¹ (AUTHOR), Liu, Yasuo¹ (AUTHOR)

Source: Mechanics of Advanced Materials & Structures. 2024, Vol. 31 Issue 24, p6015-6034. 20p.

Subject Terms: *SUPERSONIC flow, *MACH number, *SHEAR (Mechanics), *EQUATIONS of motion, *HAMILTON'S principle function, *FLUTTER (Aerodynamics)

A WENO-Based Upwind Rotated Lattice Boltzmann Flux Solver with Lower Numerical Dissipation for Simulating Compressible Flows with Contact Discontinuities and Strong Shock Waves.

Authors: Wang, Yunhao^1,2, keshitang@163.comwyh214@nuaa.edu.cn, Chen, Jiabao^1,2, chenjiabao@nuaa.edu.cn, Wang, Yan^1,2, aerowangy@nuaa.edu.cnnuaa_zyh@nuaa.edu.cn, Zeng, Yuhang^1,2, Ke, Shitang^2,3

Source: Applied Sciences (2076-3417); Dec2024, Vol. 14 Issue 23, p11450, 28p

Aerodynamic and aeroacoustic performance of a pitching foil with trailing edge serrations at a high Reynolds number.

Authors: Ji, Xueyu¹, Wang, Li¹, Ravi, Sridhar¹, Young, John¹, Lai, Joseph C. S.¹, Tian, Fang-Bao¹, f.tian@adfa.edu.au

Source: Theoretical & Computational Fluid Dynamics; Dec2024, Vol. 38 Issue 6, p825-844, 20p

Investigation of Acoustic Waves generated by the Detonation Gun of a Zenith-M modernized Powerful Antihail Station.

Authors: Ayvazyan, Gagik¹, agagarm@gmail.com, Vardanyan, Arman², vardanyan_arman@hotmail.com

Source: Engineering, Technology & Applied Science Research; Dec2024, Vol. 14 Issue 6, p17991-17995, 5p

Causal Effect of Leading-Edge Sawtooth Configuration on Flow Field Characteristics and Aerodynamic Losses in the Supersonic Compressor Cascade.

Authors: Hu, S. J.^1,2, Wei, Z. J.^1,2, weizj@sustech.edu.cn, Ni, M.^1,2, Ren, G. M.^1,2

Source: Journal of Applied Fluid Mechanics; Dec2024, Vol. 17 Issue 12, p2791-2806, 16p

Numerical Methods Comparison of Shock-Induced Separation on Transonic Axisymmetric Hump.

Authors: Zhang, Miao¹, zhangmiao@comac.cc, Tian, Zhuoyue^2,3, tianzhuoyue@mail.nwpu.edu.cn, Tang, Songxiang^2,3, tangsongxiang@163.com, Wei, Ziyan^2,3, weiziyan@mail.nwpu.edu.cn, Li, Jie^2,3, lijieruihao@nwpu.edu.cn

Source: Applied Sciences (2076-3417); Nov2024, Vol. 14 Issue 22, p10234, 20p

Effect of Spike Geometry on Drag Reduction for a Novel Combinational Spiked Blunt Body and Counter Jet Concept in Hypersonic Speeds.

Authors: Kanwar, Shyam Singh¹, shyamkanwar@gecbsp.ac.in, Agrawal, Gajendra Kumar¹, Tiwari, Shubhlakshmi², Singh, Aditya³, Dewangan, Sanjay Kumar⁴, Paikra, Ajay Kumar⁵, Shrivas, Sharda Pratap⁶

Source: Journal of Computational Analysis & Applications; 2024, Vol. 33 Issue 6, p618-627, 10p

On swirl mach number effects on acoustic-vortical waves.

Authors: Campos, LMBC¹ (AUTHOR), Lau, FJP¹ (AUTHOR) lau@tecnico.ulisboa.pt

Source: International Journal of Aeroacoustics. Nov2024, Vol. 23 Issue 7/8, p657-699. 43p.

Subject Terms: *MACH number, *SPEED of sound, *HANKEL functions, *BESSEL functions, *SWIRLING flow

Investigations of the Windage Losses of a High-Speed Shrouded Gear via the Lattice Boltzmann Method.

Authors: Dai, Yu¹, 210143@csu.edu.cn, Yang, Caihua¹, Zhu, Xiang¹, zhuxiang_csu@163.com

Source: Applied Sciences (2076-3417); Oct2024, Vol. 14 Issue 20, p9174, 17p