National Repository of Grey Literature 21 records found  beginprevious12 - 21  jump to record: Search took 0.00 seconds. 
Analysis of the supersonic flow of gas in the differentially pumped chamber EREM
Matloch, Roman ; Vyroubal, Petr (referee) ; Maxa, Jiří (advisor)
This work describes briefly electron microscopy issue and physical model of fluid flow. Then presented diploma thesis will be describing analysis and evaluation of the impact of supersonic flow on the pressure and density in the path of the primary electron beam in the differential pumping chamber. For analysis, evaluation and examination of the issue will be used CAD and CAE (Computer Aided Engineering) programs. At the same time it will be developed a methodology of calculation applicable to supersonic flow in the low pressure system at ANSYS CFX.
Aerodynamic Data for Tip Section of Rotor with 52 Titanium Blades 1375 mm Long
Luxa, Martin ; Synáč, J. ; Šimurda, David ; Šafařík, Pavel
The paper deals with aerodynamic experimental investigation of prismatic blade cascade,that represents the tip section of the rotor comprising of 52 titanium blades 1375mm long. This rotor is designed for the last stage of low pressure cylinder of a large output steam turbine. Investigated tip section is characterised by supersonic inlet, large stagger angle and supersonic outlet. Selected data from optical and pneumatic measurements are presented.
Notes to Aerodynamic Testing of Supersonic Blade Cascades
Šimurda, David ; Luxa, Martin ; Šafařík, Pavel
Relatively narrow space for aerodynamic design of long rotor blades applied at last stages of large output steam turbines often results in blades with tips operating at supersonic regimes. This brings number of problems. Main of these are additional sources of loss and rather thin border between sections operating under turbine and compressor regimes one adding to performance and the other deteriorating it. Therefore, aerodynamic cascade data on turbine blading for a range of supersonic inlet and outlet conditions are needed. However, ensuring specified supersonic conditions in a high-speed wind tunnel for blade cascade tests is not an easy task and thus it deserves attention.
Pneumatická měření na mříži TR-U-4
Šimurda, David ; Luxa, Martin ; Matějka, Milan
The research report deals with results of pneumatic measurements on blade cascade, which represents tip section of long rotor turbine blade (1375mm long - rotor disc with 52 blades).
Optická měření na mříži TR-U-4
Luxa, Martin ; Šimurda, David ; Matějka, Milan
The research report deals with results of optical measurements on blade cascade, which represents tip section of long rotor turbine blade (1375mm long - rotor disc with 52 blades).
Měřící prostor pro mříže s malým otočením proudu
Matějka, Milan ; Luxa, Martin ; Šimurda, David
The research report deals with the design of a test section for blade cascades with low flow turning. Functionality of the test section is documented by results of measurements on a tip section.
Proudové pole v měřícím prostoru pro mříže s malým otočením proudu
Šimurda, David ; Luxa, Martin ; Matějka, Milan
The research report deals with results of optical and pneumatic measurements on the tip blade cascade using test section designed for cascades with low flow turning.
Numerical and experimental inverigation of supersonic flow regimes at last stage of large output steam tip turbine cascade
Barot, M. ; Šimurda, David ; Hajšman, M. ; Tuček, A. ; Šafařík, Pavel ; Prchlík, L. ; Luxa, Martin
Paper presents some aspect of the numerical and experimental investigation of the validation of the aerodynamic performance of supersonic tip section airfoil cascade. Paper deals with limitations of various investigation methods and tries to show that advances in future development of turbomachinery can be achieved through combination of these methods.
Measurement of transonic and supersonic flow in models of rotor blades of last stage large output steam turbine
Šafařík, P. ; Luxa, Martin ; Šimurda, David
The paper deals with experimental research on transonic and supersonic flow in models of turbine cascades which represent the rotor blades of last stage large output steam turbine.
Experimentální aerodynamický výzkum jako podpora při návrhu turbostrojů
Šafařík, Pavel ; Luxa, Martin ; Šimurda, David
The paper describes a role of experimental aerodynamic research oriented to the support of the design and computauion of turbomachines. The research techniques are briefly introduced. They are namely optical measurements of flow fields and pneumatic measurements by means of traversing. Results of the high-speed aerodynamic modelling of the flow past a blade cascade cascade representing a section in the balding of the last stage of a large output steam turbine are presented.

National Repository of Grey Literature : 21 records found   beginprevious12 - 21  jump to record:
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