1-6 of 6
Keywords: guide vane
Close
Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Proceedings Papers

Proc. ASME. GT2020, Volume 10B: Structures and Dynamics, V10BT27A029, September 21–25, 2020
Paper No: GT2020-16276
... variation caused by the impact of an aero-engine fan blade is studied. Because the compressor guide vane has a small solidity, the hail may not only hit the vane when striking the blade, but also may hit the first-stage rotor blade. The effects of hail impact on the vanes and rotor blades, especially...
Proceedings Papers

Proc. ASME. GT2019, Volume 5A: Heat Transfer, V05AT11A001, June 17–21, 2019
Paper No: GT2019-90069
...Abstract Abstract The present work investigates the effects of various guide vane designs on the heat transfer enhancement of rotating U-Duct configuration with parallel 45-deg ribs. The ribs were installed on the bottom wall of the channel which has a constant heat flux boundary condition...
Proceedings Papers

Proc. ASME. GT2013, Volume 3B: Heat Transfer, V03BT13A006, June 3–7, 2013
Paper No: GT2013-94256
... Multi-field coupling method is used to assess the film-cooling properties of a turbine guide vane. The creep strain is used to evaluate the film-cooling validness, in order to take into account the effects of both temperature and thermal stress. Because of the high temperature gradients, thermal...
Proceedings Papers

Proc. ASME. GT2012, Volume 4: Heat Transfer, Parts A and B, 589-599, June 11–15, 2012
Paper No: GT2012-69521
... This study investigated convective heat transfer inside a rotating two-pass rectangular channel with guide vanes in the turning region. The objective was to determine the effect of the guide vanes on blade tip cooling. The channel had a hydraulic diameter of 26.67 mm and an aspect ratio of 5...
Proceedings Papers

Proc. ASME. GT2011, Volume 5: Heat Transfer, Parts A and B, 1351-1362, June 6–10, 2011
Paper No: GT2011-45962
... 1 Copyright © 2011 by ASME HEAT TRANSFER CHARACTERISTICS OF A NON-ROTATING TWO-PASS RECTANGULAR DUCT WITH VARIOUS GUIDE VANES IN THE TIP TURN REGION Dong Myeong Lee a, Jun Su Park a, Dong Hyun Lee a, Beom Soo Kim b and Hyung Hee Choa aDepartment of Mechanical Engineering Yonsei University, Seoul...
Proceedings Papers

Proc. ASME. GT2002, Volume 3: Turbo Expo 2002, Parts A and B, 341-347, June 3–6, 2002
Paper No: GT2002-30197
... 05 02 2009 An accurate design of a guide vane has become a major issue in gas turbine engineering since secondary flow in vane cascade has a significant effect on the end wall and airfoil suction surfaces. Heat transfer and average flow measurements were performed in a linear guide...