Static Force Measurement Technology Wind Tunnel Test

Dun Jin; Yue Ming Yang; Jie Wu; Li Min Song; Song Li

doi:10.4028/www.scientific.net/AMM.423-426.1689

Paper Titles

Nonlinear Response and Fatigue Life of Thin Plates Subjected to Non-Uniform Temperature Distributions and Acoustic Excitations
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Equilibrium of a Thick-Walled Sphere of Inhomogeneous Nonlinear-Elastic Material
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Analysis and Simulation of the Fluid Field in Thermal Water-Jet Nozzle Based on ANSYS FLUENT & ICEM CFD
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A Survey of Fluidic Thrust Vectoring Nozzle by Numerical Analysis
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Static Force Measurement Technology Wind Tunnel Test
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Application of Conjugate Heat Transfer in Multidisciplinary Design Optimization of Internal-Cooled Turbine Blade
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Numerical Simulation of Cross-Flow around Four Square Cylinders in a Square Configuration at Low Reynolds Number
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Aerodynamic Analysis of Inflatable Membrane Aeroshell
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Numerical Simulation of Boiling Flow in LNG Releasing Underwater Process
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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 423-426Static Force Measurement Technology Wind Tunnel...

Static Force Measurement Technology Wind Tunnel Test

Abstract:

Static force measurement aerodynamic wind tunnel test data provided by the aircraft normally used to predict the stall characteristics, predicted aircraft deviated,spin Sensitivities, numerical simulation of aircraft stall, spin dynamics and so on. Based on practical flight, the paper analyzed the harm of limit state flight-spin to the flight safe, emphasized the static force test techniques at high angles of attack, and obtained a series of aerodynamic test date, managed them to spin prediction analysis.

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Periodical:

Applied Mechanics and Materials (Volumes 423-426)

Pages:

1689-1692

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.423-426.1689

Citation:

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Online since:

September 2013

Authors:

Dun Jin, Yue Ming Yang, Jie Wu, Li Min Song, Song Li

Keywords:

High Angles of Attack, Spiral, Stall, Static Force Measurement, Wind Tunnel

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References

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