Results 31 to 40 of about 97,655 (378)
Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings
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]
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
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
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Integrated Numerical Simulation Research of High-speed Section in Transonic Wind Tunnel
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
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Shock Wave Capturing Numerically in Two Dimensional Supersonic Wind Tunnel for Different Configuration [PDF]
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
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Transonic buffet instability: From two-dimensional airfoils to three-dimensional swept wings
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
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
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Large-eddy simulation of laminar transonic buffet
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
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Analysis of the Transonic Buffet Characteristics of Stationary and Pitching OAT15A Airfoil
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
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Study of Separation Control of Vortex Generators on Transonic Wings
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
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