AG TURBO - GuD-Kraftwerk, 500 MW auf einer Welle, Verbundvorhaben 2.2.7: Vorderkantenausblasung bei periodisch instation...
Germany
AG TURBO - leading edge film cooling at periodic unsteady inflow conditions Final report / AG TURBO - GuD-Kraftwerk, 500...
Because of increasing aero-thermal loading of turbine blades, film cooling has to be employed to reach admissible material temperatures. The rotor-stator interaction within turbines causes periodic unsteady inflow conditions which influence the mixing process of film cooling jets and the main flow. In order to close the gap in knowledge of these in...
AG-TURBO, Turbotech II. Teilprojekte 1.326 und 1.328: Aerothermisches Verhalten von Filmkuehlungsbohrungen Abschlussberi...
Germany
Aerodynamics and cooling performance of film cooling holes Final report / AG-TURBO, Turbotech II. Teilprojekte 1.326 und...
In modern gas turbine sophisticated cooling schemes including film cooling are widely used to protect the vanes and blades of the first turbine stages from failure and to achieve high life-cycles. In film cooling applications, injection from discrete holes is commonly used to generate a coolant film on the blade's surface. To ensure a good protecti...
HTGT-TURBOTECH II, Vorhaben 1.327. Filmgekuehlte Turbinenplattformen Schlussbericht
Germany
Filmgekuehlte Turbinenplattform in transsonischem Stroemungsfeld
Germany
HTGT-TURBOTECH II, Vorhaben 1.327. Filmgekuehlte Turbinenplattformen Schlussbericht
Germany
Aerodynamik von filmgekuehlten Turbinenschaufeln bei unterschiedlicher Kuehlkonfiguration Kurzfassung des Abschlussberic...
Germany
Aerodynamics of film-cooled turbine blades with different cooling configurations Short version of the final report of th...
The effects of different cooling configuration on the aerodynamics of film-cooled turbine blades were investigated systematically. Both the effects on the rotor flow of blowout at the back edge of the guide blade and the interactions between cooling air blowout in the rotor and periodically fluctuating inflow were to be analyzed. The project compri...
HTGT-TURBOTECH II, Vorhaben 1.327. Filmgekuehlte Turbinenplattformen Schlussbericht
Germany
