Results 31 to 40 of about 97,655 (378)

Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings

open access: yesAIAA Journal, 2018
Since its introduction, the NASA Common Research Model has proved a useful aerodynamic benchmark for predicting computational-fluid-dynamics-based drag and aerodynamic design optimization.
Timothy R. Brooks, G. Kenway, J. Martins
semanticscholar   +1 more source

Periodic transonic flow and control [PDF]

open access: yesThe Aeronautical Journal, 2008
AbstractThe current understanding of periodic transonic flow is reviewed briefly. The effects of boundary-layer transition, non-adiabatic wall conditions and modifications to the aerofoil surface geometry at the shock interactions on periodic transonic flow are discussed.
Raghunathan, Srinivasan   +4 more
openaire   +4 more sources

Characteristic prediction method of transonic axial flow turbine

open access: yesZhongguo Jianchuan Yanjiu, 2021
ObjectivesRegarding transonic flow occurring at the throat of the stator blades of axial flow turbines at high subsonic and transonic speeds, it is will need a long period of time to have 3D reseach and to obtain the characteristic parameters. Therefore,
Yufeng DU, Jie GAO, Qun ZHENG, Guojun MA
doaj   +1 more source

Integrated Numerical Simulation Research of High-speed Section in Transonic Wind Tunnel

open access: yesHangkong gongcheng jinzhan, 2020
For civil aviation aircraft with high subsonic economic cruising and fighter with high maneuverability at transonic speed, their demand for high-performance transonic wind tunnels is becoming more and more urgent, and integrated numerical simulation ...
YANG Xiaochuan   +5 more
doaj   +1 more source

Shock Wave Capturing Numerically in Two Dimensional Supersonic Wind Tunnel for Different Configuration [PDF]

open access: yesEngineering and Technology Journal, 2012
Numerical solutions of two dimensional Euler equations are obtained for transonic and supersonic flows. The shock capturing method is employed to solve compressible Euler equations by using MacCormack's time marching method that an explicit finite ...
Ahmed Fouad Mahdi
doaj   +1 more source

Transonic buffet instability: From two-dimensional airfoils to three-dimensional swept wings

open access: yesPhysical Review Fluids, 2019
The objective of the present study is to explain the evolution of the transonic buffet phenomenon from two-dimensional airfoils to three-dimensional swept wings by a global stability analysis.
E. Paladini   +4 more
semanticscholar   +1 more source

Drag Reduction on the Basis of the Area Rule of the Small-Scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology (Second Report)

open access: yesAerospace
A small-scale supersonic flight experiment vehicle named OWASHI is being developed at Muroran Institute of Technology as a flying testbed for verification of innovative technologies for high-speed atmospheric flights.
Kazuhide Mizobata   +2 more
doaj   +1 more source

Large-eddy simulation of laminar transonic buffet

open access: yesJournal of Fluid Mechanics, 2018
A large-eddy simulation of laminar transonic buffet on an airfoil at a Mach number $M=0.735$ , an angle of attack $\unicode[STIX]{x1D6FC}=4^{\circ }$ , a Reynolds number $Re_{c}=3\times 10^{6}$ has been carried out.
J. Dandois, I. Mary, V. Brion
semanticscholar   +1 more source

Analysis of the Transonic Buffet Characteristics of Stationary and Pitching OAT15A Airfoil

open access: yesApplied Sciences
Transonic buffet flow is a classical complex and unstable flow that has a negative effect on aircraft fly safety. Therefore, it is crucial to study the unsteady characteristics of buffet flow. The numerical analysis method is very useful in achieving the
Xueyuan Nie   +5 more
doaj   +1 more source

Study of Separation Control of Vortex Generators on Transonic Wings

open access: yesJournal of Fluid Science and Technology, 2011
Flows around vortex generators (VGs), which serve as one of the important flow control methods, are investigated by solving Reynolds-Averaged Navier-Stokes (RANS) equations. The influences on the main flow of VGs are intended to explore.
Jingbo HUANG   +3 more
doaj   +1 more source

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