Zobrazeno 1 - 10
of 40
pro vyhledávání: '"R. Benay"'
Publikováno v:
Shock Waves. 22:385-402
The possibility of creating unsteady distortions of the tip shock by waves emitted from an aircraft is assessed experimentally. The model chosen is a cylindrical fore body equipped with a spike. This configuration is known for generating an important
Design of a boundary layer suction device for a supersonic quiet wind tunnel by numerical simulation
Autor:
B. Chanetz, R. Benay
Publikováno v:
Aerospace Science and Technology. 8:255-271
The paper deals with a numerical contribution for a realization of a quiet supersonic wind tunnel. It is known that upstream of the test-section, acoustic noise originating from the turbulent boundary layer of the nozzle walls has an influence on the
Autor:
R. Benay
Publikováno v:
Experiments in Fluids. 54
A novel calibration method of multi-hole pressure probes is presented. The case of a particular in-house seven-hole probe is treated explicitly. The three components of the velocity vector are recovered by minimising the difference between the pressu
Publikováno v:
Drag Reduction by Shock and Boundary Layer Control ISBN: 9783642077623
The aim of this study was to investigate in detail the flow field resulting from transonic shock wave / boundary layer interactions under control conditions. Several control techniques have been investigated: 1) active control consisting in sucking a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::45e64c76358d1228100b21a54a446b45
https://doi.org/10.1007/978-3-540-45856-2_3
https://doi.org/10.1007/978-3-540-45856-2_3
Publikováno v:
Shock Waves; May2003, Vol. 12 Issue 6, p469, 9p
Publikováno v:
15th Atmospheric Flight Mechanics Conference.
Publikováno v:
5th Applied Aerodynamics Conference.
Publikováno v:
Turbulent Shear-Layer/Shock-Wave Interactions ISBN: 9783642827723
The paper presents the first results of a thorough experimental analysis of a strong 3D shock-wave/turbulent boundary-layer interaction occurring in a channel. Many field measurements have been performed by using a 3 component LDV system. The results
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f7a57092878d6c2f2597d4037989c72b
https://doi.org/10.1007/978-3-642-82770-9_22
https://doi.org/10.1007/978-3-642-82770-9_22
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