Александр Плесной » Публикация

Lavrenchenko G.K. Plesnoy A.V. (2013). Increasing the efficiency of the gas-expansion machine-compressor units used in the structure of the air-separating installations of medium pressure// Tekhnicheskie Gazy. [Industrial Gases]. — No. 4. — P. 18-23. (Rus.). Lavrenchenko G.K. Plesnoy A.V. (2013). The optimization of the multi-shaft expander-compressor unit of the air separation unit of medium capacity// Tekhnicheskie Gazy. [Industrial Gases]. — No. 5. — P. 15-24. (Rus.). Lavrenchenko G.K., Plesnoy A.V. (2012). Research of work expander-compressor units with two stages extensions in composition medium pressure ASU// Tekhnicheskie Gazy. [Industrial Gases]. — № 6. — P. 34-41. (Rus.). Epifanova V.I. (1998). Compressor and expander radial turbo machine. — Moskow: Bauman Moskow State Technical University. — 624 p. (Rus.). Taran V.N. (2003). Prediction of the cryogenic turbo expander characteristics// Tekhnicheskie Gazy. [Industrial Gases]. — № 4. — P. 28-38. (Rus.). Brown R. N. (2011). Compressors: Selection and Sizing. — Elsevier. — 620 р. Galerkin Yu.B., Soldatova K.V., Titenskiy V.I. (2007). The theory, calculation and design of compressor machines dynamic action. Turbocompressors. — Sanсt-Peterburg: SPbGPU. — 142 p. (Rus.). Boyko L.G. Barysheva E.S. (2011). Transonic flow research in high-pressure centrifugal impeller// Vestnik dvigatelestroeniya. [Нerald Engine Building]. — №. 2. — P. 203-207. (Rus.). Krain H. (2002). Unsteady Diffuser Flow in a Transonic Centrifugal Compressor// Intrn. Journal of Rotating Machinery. — V. 8. — No. 3. — P. 223-231. Krain H., Hoffmann B. (2008). Flow Study of a Redesigned High-Pressure-Ratio Centrifugal Compressor// Journal of Propulsion and Power. — V. 24. — No. 5. — P. 1117-1123. Bulot N., Trebinjac I. (2008). Effect of the unsteadiness on the diffuser flow in a transonic centrifugal compressor stage// Inter. Journal of Rotating Machinery. — Article ID 932593. — P. 1-11. Fleming R., Lou F., Key N. L. (2011). The Development of a High Speed Centrifugal Compressor Research Facility// 49th AIAA Aerospace Sciences Meeting. — V. 7. — P. 4-7.