Model-based stagnation pressure control in a supersonic wind tunnel [PDF]
FME Transactions, 2016 The flow parameters control in wind tunnels is an area of intense research in recent years, with the aim of improving quality and efficiency of the wind tunnel operation.
Ilić Biljana +3 more
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Numerical Investigation of a Supersonic Wind Tunnel Diffuser Optimization
AerospaceThe objective of this study is to enhance the methodology for the design of a supersonic wind tunnel, improving the process with advanced computational techniques.
Riccardo Nicoletti +7 more
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Journal of Fluid Science and Technology, 2014 The objective of this study is to improve the performance of the sensitivity-adjustable three component force balance developed in the previous study for the usage of various experimental conditions.
Gouji YAMADA +4 more
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Photogrammetry for accurate model deformation measurement in a supersonic wind tunnel [PDF]
Experiments in Fluids, 2018 The interest in adaptive devices for high-speed applications leads to the need for an accurate and reliable technique to obtain model deformation measurements during experiments.
Michela Gramola +2 more
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Design and CFD Simulation of Supersonic Nozzle by Komega turbulence model for Supersonic Wind Tunnel [PDF]
E3S Web of ConferencesThis paper presents an impressive design of a convergent divergent (C-D) nozzle using the method of characteristics for a Mach number 2 test section. The nozzle’s geometry was meticulously crafted in SolidWorks, and its performance was evaluated through ...
Raman Ravi Shankar +6 more
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Convergence of transonic wind tunnel test results of the AGARD-B standard model [PDF]
FME Transactions, 2020 AGARD-B is a widely-used configuration of a standard wind tunnel model. Beside its originally intended application for correlation of data from supersonic wind tunnel facilities, it was tested in a wide range of Mach numbers and, more recently, used for ...
Damljanović Dijana +3 more
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Development of air to air ejector for supersonic wind tunnel
EPJ Web of Conferences, 2014 The contribution deals with the development of design of new conception of ejector with twelve primary annular nozzles arranged around the inlet part of the mixing chamber. The ejector is proposed to be used for propulsion of supersonic experimental wind
Kracík Jan +2 more
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Plume and Shock Interaction Effects on Sonic Boom in the 1-foot by 1-foot Supersonic Wind Tunnel [PDF]
, 2015 Raymond Castner +3 more
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The control system design and study for continuous supersonic wind tunnel
Xibei Gongye Daxue Xuebao, 2022 As the first continuous supersonic wind tunnel in China, Mach number and total pressure are the most important flow field parameters of the wind tunnel, how to precise control and rapid and stable adjustment of total pressure and Mach number is the key ...
CHEN Dan +4 more
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SHAPE OPTIMIZATION OF SUPERSONIC WIND TUNNEL DIFFUSER USING GENETIC ALGORITHM [PDF]
مجله مدل سازی در مهندسی, 2012 Wind tunnel, as an experimental laboratory, has many applications nowadays. Installation of wind tunnel is very expensive, so designers try to reduce wind tunnelâs installation and test costs by optimizing the design of various components of the wind ...
مرتضی Javadpour +2 more
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