WebLaser anemometer surveys were made of the 3-D flow field in NASA rotor 67, a low aspect ratio transonic axial-flow fan rotor. The test rotor has a tip relative Mach number of 1.38. The flowfield was surveyed at design speed at near peak efficiency and near stall operating conditions. Data is presented in the form of relative Mach number and relative flow angle … WebFind company research, competitor information, contact details & financial data for DATATRANSONIC LIMITED of FELTHAM. Get the latest business insights from Dun & …
Transonic Data Technology Corp. Company Profile
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NTRS - NASA Technical Reports Server
WebKey pieces of literature and technical data for Transonic Inside . Key pieces of literature and technical data for Transonic Inside This website stores cookies on your computer. … WebJan 4, 2024 · The physics of the complex transonic flow includes shock-induced separation and modes of shock oscillation, and they have also compared the buffeting phenomenon between 2 and 3D flows. Very recently, Gao and Zhang ( 2024) have revised the transonic aeroelasticity-related works carried out so far. WebFeb 1, 1999 · The tip clearance flows of transonic compressor rotors are important because they have a significant impact on rotor and stage performance. A wall-bounded shear layer formed by the relative motion between the overtip leakage flow and the shroud wall is found to have a major influence on the development of the tip clearance flow field. This shear … heart of darkness play online