Entropy Stable DGSEM Schemes of Gauss Points Based on Subcell Limiting. [PDF]
Entropy (Basel), 2023 Liu Y, Zhu H, Yan ZG, Jia F, Feng X.
europepmc +1 more source
Structure Design of the Force Testing Central Support of a Transonic and Supersonic Wind Tunnel
Jixie chuandong, 2015 The force testing central support is an important part of the model supporting system in a transonic & supersonic wind tunnel,the performance of which is qualified or not would directly affect the control of model attitude angel during wind tunnel ...
Dong Bin +3 more
doaj
Molecular Oncology, Volume 20, Issue S1, Page 1-692, August 2026.Abstracts submitted to the ‘EACR 2026 Congress: Innovative Cancer Science’, from 08–11 June 2026 and accepted by the Congress Organising Committee are published in this Supplement of Molecular Oncology, an affiliated journal of the European Association for Cancer Research (EACR).
wiley +1 more source
Effect of Leading-Edge Erosion on the Performance of Transonic Compressor Blades
International Journal of Turbomachinery, Propulsion and PowerIn this paper, an experimental and numerical investigation of the effect of leading-edge erosion in transonic blades was performed. The measurements were carried out on a linear blade cascade in the Transonic Cascade Wind Tunnel of DLR in Cologne at two ...
Alexander Hergt +5 more
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Characterization of Supersonic Compressible Fluid Flow Using High-Speed Interferometry. [PDF]
Sensors (Basel), 2021 Psota P +10 more
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Euler flow solutions for transonic wind tunnel section
, 1990 Steady, 2D Euler flow computations have been performed for a wind tunnel section, designed for research on transonic shock wave - boundary layer interaction. For the discretization of the steady Euler equations, an upwind finite volume technique has been applied.
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Linearized Theory of Wind Tunnel Interference at Transonic Speed
The Journal of the Japan Society of Aeronautical Engineering, 1956 It has been proved that a linearized theory is consistent for three dimensional lifting case at sonic and nearly sonic speeds and is also applicable to a nonlifting case in the field of Mach number nearly one which has boundaries at finite distances.
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Automatic Attitude Setting of a Wind Tunnel Model in a Transonic Wind Tunnel
Automatic Attitude Setting of a Wind Tunnel Model in a Transonic Wind TunnelA description of an improved automatic attitude setting system, of a wind tunnel model in a 2m×2m transonic wind tunnel is presented. The purpose of this improvement is to save on manpower, and shorten the access time for setting from one testing condition to another. An 8K words mini-computer is employed, to control the electirically powered mechanism
openaire
Skin-Friction-Based Identification of the Critical Lines in a Transonic, High Reynolds Number Flow via Temperature-Sensitive Paint. [PDF]
Sensors (Basel), 2021 Costantini M +3 more
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Miniaturization and Model-Integration of the Optical Measurement System for Temperature-Sensitive Paint Investigations. [PDF]
Sensors (Basel), 2023 Lemarechal J +4 more
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