Investigation of the Starting Process of a Supersonic Wind Tunnel
Bulletin of JSME, 1980 The starting process of a supersonic wind tunnel with a diffuser with contraction has been studied in detail by schlieren optical observations and pressure measurements. As the result, it has been shown that the wind tunnel starts when the flow is even sonic but not choked at the second throat.
Kazuyasu Matsuo +3 more
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Supersonic and transonic Mach probe for calibration control in the Trisonic Wind Tunnel [PDF]
INCAS Bulletin, 2017 A supersonic and high speed transonic Pitot Prandtl is described as it can be implemented in the Trisonic Wind Tunnel for calibration and verification of Mach number precision. A new calculation method for arbitrary precision Mach numbers is proposed and
Alexandru Marius PANAIT
doaj +2 more sources
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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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
doaj +2 more sources
Experimental investigation of a newly designed supersonic wind tunnel [PDF]
Progress in Flight Physics – Volume 7, 2015 The flow characteristics of the tandem nozzle supersonic wind tunnel at the Institute of Fluid Mechanics, Technische Universitat Braunschweig, a are investigated. Conventional measurement techniques were utilized. The flow development is examined by pressure sensors installed at various streamwise positions.
Rolf Radespiel, Jie Wu
openaire +3 more sources
Wind Tunnel Testing on Start/Unstart Characteristics of Finite Supersonic Biplane Wing [PDF]
, 2013 This study describes the start/unstart characteristics of a finite and rectangular supersonic biplane wing. Two wing models were tested in wind tunnels with aspect ratios of 0.75 (model A) and 2.5 (model B). The models were composed of a Busemann biplane
Hiroshi Yamashita +6 more
openalex +2 more sources
Shape optimization of supersonic ejector for supersonic wind tunnel
Applied and Computational Mechanics, 2010 The article deals with the shape optimization of a supersonic ejector for propulsion of an experimental supersonic wind tunnel. This ejector contains several primary nozzles arranged around the mixing chamber wall. CFD software Fluent was used to compute
Dvořák V.
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Aerodynamical behavior of spherical debris in the supersonic and rarefied wind tunnel MARHy
, 2020 Nicolas Rembaut +2 more
openalex +3 more sources
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
doaj +1 more source
Integrated approach to gas-dynamic designing of supersonic air intakes of aircraft
Aviation, 2021 The analytical and experimental studies of the aircraft’s supersonic air intakes have been carried out. An integrated approach to the gas-dynamic designing of aircraft’s supersonic air intakes that eliminates the scale effect problem of a wind tunnel ...
Aleksey Kornev +4 more
doaj +1 more source