Литература

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1. Relative Performance Comparison Between Baseline Labyrinth and Dual-Brush Compressor Discharge Seals in a YT-700 Engine Test / R.C. Hendricks, T.A. Griffin, T.R. Kline, K.R. Csavina, A. Pancholi, D. Sood. – NASA Technical Memorandum 106360, 1994. – 23 p.

2. Demiroglu M. An investigation of heat generation characteristics of brush seals / M. Demiroglu, J. ATichy. – ASME Turbo Expo2007, GT 2007-28043. – 10 p.

3. Design features and performance details of brush seals for turbine applications / M. Neef, E. Salda, N. Surken, J. Walkehorst. – ASME Turbo Expo 2006, GT 2006-90404. – 8 p.