Research Journal of Applied Sciences

Year: 2014
Volume: 9
Issue: 10
Page No. 684 - 690

Investigation of the Effect of the Gas Turbine Compressor Supports on Gas Flow Circumferential Nonuniformity

Authors : Aleksandr I. Ermakov, Aleksandr O. Shklovets, Grigorii M. Popov and Daria A. Kolmakova

References

Bochkarev, S.K., A.Y. Dmitriev, V.V. Kulagin, S.V. Makeenko, V.V. Mosoulin and A.A. Mossoulin, 1993. Experience and problems of computer aided thermogasdynamic analysis of testing results for gas-turbine engines with complex schemes. Aviatsionnaya Tekhnika, 2: 68-70.

Korzh, N.D., V.V. Kulagin and V.D. Bonzin, 1973. Influence of air bleeding and leakage on twin-spool bypass turbojet engine parameters. Soviet Aeronautics, 16: 96-99.

Korzh, N.D., V.V. Kulagin, V.D. Ronzin and N.A. Gachegov, 1973. Turbine inlet temperature of two-spool high-temperature turbofan. Soviet Aeronautics, 16: 61-63.

Kuz'michev, V.S. and M.A. Morozov, 1991. Conception of method of pattern recognition of working process of gas turbine engines in conditions of information deficit. Soviet Aeronautics, 3: 44-49.

Kuz'michev, V.S., 2012. Simulation of an aircraft flight within the issues of the workflow parameters optimization concerning gas turbine engines. The Samara Scientific Center of the Russian Academy of Sciences Bulletin, Volume 14, No. 2, pp: 491-494.

Maslov, V.G., S.K. Bochkarev and V.S. Kuz'michev, 1976. Influence of flight vehicle mission on optimal gas turbine engine parameters. Soviet Aeronautics, 19: 54-59.

Shklovets, A.O., G.M. Popov and D.A. Kolmakova, 2012. Issues of numerical investigations of forced axial compressor blades oscillations. Vestnik Dvigatelestroeniya, 2: 223-227.

Shklovets, A.O., G.M. Popov and D.A. Kolmakova, 2013. Optimization of the compressor stage blading of gas turbine engine to ensure the dynamic strength in rotor blade row. Vestnik Dvigatelestroeniya, 2: 192-197.

Zhukov, O.M., V.S. Kuz'michev, A.N. Kovartsev, M.A. Morozov and B.D. Fishbein, 1985. Exhaust system configuration evaluation as a subsystem of aircraft system based on engine transport effectiveness. Soviet Aeronautics, 28: 105-109.

Design and power by Medwell Web Development Team. © Medwell Publishing 2024 All Rights Reserved