THE RESULTS OF THE IMPROVEMENT OF THE STAGE OF HIGHLY LOADED LOW PRESSURE TURBINE
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Harvey, N. W., Cox, J. C., Schulte, V., Howell, R., Hodson, H. P. The Role of Research in the Aerodynamic Design of an Advanced Low-Pressure Turbine. Proc. Instn. Mech. Engr., 1999, vol. 213, Part A.
De Poli, P., Frola, G., Gallizio, M., Fattore, L., Mattone, M. Multi-disciplinary Integration and Robustness Evaluation Applied to Low Pressure Turbine Casing Design. ASME Pap. GT2006-90464.
Bertini, F., Credi, M., Marconcini, M., Giovannini, M. Path Towards the Aerodynamic Robust Design of Low Pressure Tutbines. ASME Pap, GT2012-69456.
Horlock, J. H. Axial flow turbines: Fluid mechanics and Thermodynamics. London, Butterworths, 1966. 286 p. (Russ. ed.: Khorlok, Dzh. Kh. Osevye turbiny: gazovaya dinamka i termodinamika. Moscow, Mashinostroenie Publ., 1972. 284 p.).
Vázquez, R., Cadrecha, D., Torre, D., Vázquez, R. High stage loading low pressure turbine. A new proposal for an efficiency chart. ASME Pap, GT2003-38374.
Deych, M. E., Filippov, G. A., Lazarev, L. Ya. Atlas profiley reshetok osevykh turbin [Atlas of axial flow turbine lattice of profiles]. Moscow, Mashinostroenie Publ., 1965. 96 p. (In Russian).
Venediktov, V. D., Granovskiy, A. V., Karelin, A. M., Kolesov, A. N., Mukhtarov, M. Kh. Atlas eksperimental'nykh kharakteristik ploskikh reshetok okhlazhdaemykh gazovykh turbin [Atlas of experimental characteristics of flat lattices of cooled gas turbines]. Moscow, TsIAM, 1990. 393 p. (In Russian).
Mamaev, B. I., Klebanov, A. G. Profil'nye poteri v turbinnoy reshetke [Profile losses in the turbine lattice]. Teploenergetika, 1970, no. 6, pp. 38-42. (In Russian).
Khomylev, S. A., Reznik, S. B., Ershov, S. V. Chislennoe issledovanie obtekaniya turbinnykh reshetok profiley: Chast' 2 Issledovanie kharakteristik vysokonagruzhennykh reshetok [Numerical study of flow in turbine profiles lattices: Part 2 Investigation of the characteristics of high-loaded lattices]. Aviatsionno-kosmicheskaya tekhnika i tekhnologiya Publ. – Aerospace technic and technology, 2008, no. 8 (55), pp. 46-50. (In Russian).
Khomylev, S. A., Rudenko, V. T., Lyusina, A. V. Chislennoe issledovanie vliya-niya formy peredney kromki na effektivnost' turbinnoy reshetki [Numerical study of the influence of the leading edge shape on the efficiency of a turbine blade]. Vіsnik Natsіonal'nogo tekhnіchnogo unіversitetu “Kharkіvs'kiy polіtekh-nіchniy іnstitut”, zb. nauk. pr. [Bulletin of the National Technical University "KhPI"]. Khar'kov, 2011, no. 5, pp. 45-50. (In Russian).
Khomylev, S. A., Reznik, S. B., Ershov, S. V. Rezul'taty aerodinamicheskogo usovershenstvovaniya profilya vysokonagruzhennoy turbinnoy reshetki [Results of the aerodynamic improvement of the profile of a high-loaded turbine blade]. Aviatsionno-kosmicheskaya tekhnika i tekhnologiya – Aerospace technic and technology, 2010, no. 7 (74), pp. 57-61. (In Russian).
Ershov, S. V. Programmnyy kompleks dlya rasche-ta prostranstvennykh techeniy vyazkogo gaza v re-shetkakh turbomashin [A software package for calculating the three dimensional flow of a viscous gas in turbomachine lattices]. Problemy mashinostroeniya, 2012, vol. 15, no. 34, pp. 52- 60. (In Russian).
Menter, F. R. Two-equation eddy viscosity turbulence models for engineering applications. AIAA J., 1994, vol. 32, no. 11, pp. 1299–1310.
Karelin, A. M. Postroenie reshetki turbinnykh profiley na osnove ratsional'nykh parametricheskikh krivykh. Lopatochnye mashiny i struynye apparaty [Construction of the turbine profile lattice on the basis of rational parametric curves. Blade machines and jet apparatus], Moscow, Trudy TsIAM, 1989, vol. 9, no. 1234, pp. 79-89. (In Russian).
Nguen, A. K., Lapshin, K. L. Kharakteristiki i struktura potoka turbinnoy stupeni s otritsatel'nym gradientom stepeni reaktivnosti [Characteristics and structure of the flow in a turbine stage with a negative gradient of the degree of reactivity] Nauchno-tekhnicheskie vedomosti SPbGPU, 2016, no. 2 (243), pp. 163-173. (In Russian).
DOI: https://doi.org/10.32620/aktt.2019.5.04