Search Results - "Mach number"

Aeroelastic Effects on the Internal Flow Characteristics and Performance of the S-Shaped Inlet Duct.

Authors: Liao, Daxin Wang, Hexiang Xiong, Neng et al.

Source: Applied Sciences (2076-3417); May2026, Vol. 16 Issue 10, p5033, 21p

Experimental Study on the Effect of Leading-Edge Curvature Optimization on Pressure Fluctuations in Transonic Compressor Blades.

Authors: Yang, Ye Hong, Shaozun Yi, Yuan et al.

Source: Applied Sciences (2076-3417); May2026, Vol. 16 Issue 10, p4872, 20p

Scramjet motorunun değişen irtifa ve Mach sayılarında incelenmesi.

Alternate Title: Investigation of a scramjet engine at varying altitudes and Mach numbers.

Authors: Turmuş, Ahmet Özdamar, Aydoğan

Source: Journal of the Faculty of Engineering & Architecture of Gazi University / Gazi Üniversitesi Mühendislik Mimarlık Fakültesi Dergisi,. Mar2026, Vol. 41 Issue 1, p47-62. 16p.

Subjects: Scramjet engines, Mach number, Hydrogen as fuel, Thermodynamics, Combustion efficiency, Fluid dynamics, Geopotential height

Numerical Simulation and Experimental Study of Flow Field and Aerodynamic Characteristics of a Trajectory Correction Projectile with Air-ducts Structure.

Authors: Cui, S. L. Huang, Y. L. Yang, Y. et al.

Source: Journal of Applied Fluid Mechanics; Mar2026, Vol. 19 Issue 3, p464-481, 18p

Bifurcation in compressible moving fluids and suppressing atmospheric turbulence of aircraft-flow amplifies sound.

Authors: Qian, Zuwen¹, qianzw@mail.ioa.ac.cn

Source: Sound & Vibration; 2026, Vol. 60 Issue 2, p1-24, 24p

Study on hypersonic forebody transition characteristics based on the amplification factor transport model.

Authors: Yuan, Xu Haiyang, Wang Chengyu, Wang et al.

Source: Acta Aerodynamica Sinica / Kongqi Donglixue Xuebao. Mar2026, Vol. 44 Issue 3, p166-178. 13p.

Passive control of suddenly expanded flow and temperature distribution along the duct at critical Mach number.

Authors: Tamboli, Shahid Bellary, Sayed Ahmed Imran Abdullah, Roslinda et al.

Source: Scientific Reports. 1/7/2026, Vol. 16 Issue 1, p1-46. 46p.

Application Exploration of Flow Field Prediction in Free Jet Tests Based on Proper Orthogonal Decomposition Method.

Authors: Wang, Juanjuan Su, Weiyi Liu, Zhiyou et al.

Source: Applied Sciences (2076-3417); Jan2026, Vol. 16 Issue 1, p230, 17p

NUMERICAL INVESTIGATION OF TRANSONIC SHOCK WAVE CHARACTERISTICS ON SUPERCRITICAL AIRFOILS UNDER VARIOUS FLOW CONDITIONS.

Authors: KAYA, Mehmet Numan¹, mnkaya@erbakan.edu.tr

Source: Konya Journal of Engineering Sciences / Konya Mühendislik Bilimleri Dergisi; Dec2025, Vol. 13 Issue 4, p1252-1263, 12p

Characteristic variation of Mach number in subsonic co-flowing jets by varying lip thickness.

Authors: Kumar, K. Sathish Shankar, R. Naren Ganesan, V. G. et al.

Source: Scientific Reports. 11/26/2025, Vol. 15 Issue 1, p1-19. 19p.

Shock Mach Number Effect on Instability Evolution at a Light–Heavy Fluid Interface: A Numerical Investigation.

Authors: Alsaeed, Salman Saud Singh, Satyvir Alshammari, Nahar F.

Source: Axioms (2075-1680). Nov2025, Vol. 14 Issue 11, p813. 34p.

再入轨道下的高焓稳定性分析及电离的影响.

Alternate Title: Stability analysis of high-enthalpy boundary layers during reentry and the effects of ionization.

Authors: 鲁锐洋 黄章峰

Source: Acta Aerodynamica Sinica / Kongqi Donglixue Xuebao. Nov2025, Vol. 43 Issue 11, p56-65. 10p.

Lip Thickness Effect on Coaxial Subsonic and Correctly Expanded Sonic Jet Mixing.

Authors: Angelin, Irish Narenshankar, R. Sathishkumar, K. et al.

Source: International Journal of Vehicle Structures & Systems (IJVSS). 2025, Vol. 17 Issue 5, p766-771. 6p.

Subjects: Mach number, Subsonic flow, Jet engines, Pressure drop (Fluid dynamics), Flow velocity

Theoretical and numerical investigation of wedge and cone nose profiles at supersonic speed.

Authors: Kumar, Uttam Kumar, Rakesh

Source: Numerical Heat Transfer: Part A -- Applications. 2025, Vol. 86 Issue 15, p5329-5353. 25p.

Subjects: Mach number, Compressibility (Fluids), Aerodynamic load, Kinetic energy, Projectiles, Shock waves

CFD-Driven Enhancement for Supersonic Aircraft Variable Geometry Inlet.

Authors: Ezzeldin, Abdullah Wu, Zhenlong

Source: Applied Sciences (2076-3417); Sep2025, Vol. 15 Issue 17, p9825, 25p

Numerical Simulation of Coupled CFD-flight Mechanics and Taguchi’s Approach for Reliability and Safety Assessments in the Hot Stage Separation of a Launch Vehicle.

Authors: Nasiri, D. Adami, M. Taei, H. et al.

Source: Journal of Applied Fluid Mechanics; Aug2025, Vol. 18 Issue 8, p2085-2094, 10p

Effect of Combined Kappa–Cairns distributed electrons on ion-acoustic solitary structures in electron–ion dusty plasma.

Authors: Pain, Rittika Bandyopadhyay, Anup Dalui, Sandip et al.

Source: Zeitschrift für Naturforschung Section A: A Journal of Physical Sciences. Aug2025, Vol. 80 Issue 8, p705-717. 13p.

Analysis of the Limiting Values of Thermodynamic Parameters for Jouguet Detonation.

Authors: Avramenko, Andriy A. Shevchuk, Igor V. Kovetskaya, Margarita M. et al.

Source: Mathematics (2227-7390). Aug2025, Vol. 13 Issue 15, p2419. 18p.

A study of initial conditions' effects on thermal properties of compressible homogeneous sheared non-isentropic turbulence using rapid distortion theory (RDT).

Authors: Riahi, Mohamed Lili, Taieb

Source: Canadian Journal of Physics; May2023, Vol. 101 Issue 5, p211-221, 11p

Aerodynamic design optimization of a NACA 0012 airfoil: An introductory adjoint discrete tool for educational purposes.

Authors: Ntantis, Efstratios L. Xezonakis, Vasileios

Source: International Journal of Mechanical Engineering Education. Jul2025, Vol. 53 Issue 3, p611-630. 20p.

Subjects: Mach number, Reynolds number, Derivatives (Mathematics), Structural optimization, Educational objectives