naa a22 4500 510761615 CHVBK 20180411083141.0 cr unu---uuuuu 180411e20130301xx s 000 0 eng 10.1134/S0040601513020055 doi (NATIONALLICENCE)springer-10.1134/S0040601513020055 The influence of a special fillet between the endwall and airfoil at the leading edge on the performance of the turbine nozzle diaphragm [Elektronische Daten] [B. Mamaev, R. Saha, J. Fridh] It is shown from the results of experimental investigations carried out on a nozzle diaphragm's sector that an enlarged fillet at the vane leading edge does not have an essential effect on the flow and energy losses in the nozzle diaphragm. Pleiades Publishing, Ltd., 2013 nozzle diaphragm nationallicence fillet nationallicence end losses nationallicence flow exit angle and vortex structure nationallicence Mamaev B. OOO Siemens, Bol'shaya Tatarskaya ul. 9, Room 4.18, 115184, Moscow, Russia aut Saha R. Royal Technological Institute, SE-10044, Stockholm, Sweden aut Fridh J. Royal Technological Institute, SE-10044, Stockholm, Sweden aut Thermal Engineering SP MAIK Nauka/Interperiodica 60/3(2013-03-01), 217-222 0040-6015 60:3<217 2013 60 11509 https://doi.org/10.1134/S0040601513020055 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1134/S0040601513020055 text/html Onlinezugriff via DOI NATIONALLICENCE 700 1- Mamaev B. OOO Siemens, Bol'shaya Tatarskaya ul. 9, Room 4.18, 115184, Moscow, Russia aut NATIONALLICENCE 700 1- Saha R. Royal Technological Institute, SE-10044, Stockholm, Sweden aut NATIONALLICENCE 700 1- Fridh J. Royal Technological Institute, SE-10044, Stockholm, Sweden aut NATIONALLICENCE 773 0- Thermal Engineering SP MAIK Nauka/Interperiodica 60/3(2013-03-01), 217-222 0040-6015 60:3<217 2013 60 11509 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer