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Title
Authors
Main approaches and features of the design of aircraft hydro-mechanical control systems
Petrov P.V., Tselischev V.A., Kuderko D.A.
Analysis of technological parameters of production (methodological aspect)
Sosnina T.N.
Estimation of the adequacy of electronic flow model and efficiency characteristic of small centripetal turbine drive
Matveev V.N., Shabliy L.S.
Test benches for researching the processes and operational development of low emission gas turbine engine combustion chambers
Markushin A.N., Baklanov A.V.
State science and technology policy in the Soviet Union during the pre-war period
Bannikova N.F.
Experimental research and selection of design parameters of the onboard microaccelerations state and compensation monitoring equipment on the low-orbit space microgravitational platform
1 1.
Research of machinability of heat resistant steels 10Х11НN23T3MР-ВД used in parts of gas turbine engines
Surkov O.S., Kondratiev A.I., Alexeev V.P., Haymovich A.I.
Consideration of active forces at internal-combustion engine analysis in MSC.ADAMS environment
1 1., 1 1., 1 1.
Modeling and experimental research of the multi-level drawing and geometric training system
Ivashchenko V.I.
Development of methods of carrying out experimental research of measurement errors for sets of geometrical parameters on NC equipment as in the case of a turbine disk
Bolotov M.A., Alexeev V.P., Pronichev N.D.
Research of methods for protection the surface of cryogenic tanks from ice formation
1 1., 1 1., 1 1.
Methodological and analytical support for the creation and maintenance of aerospace industry technological development strategic programs
Gaponenko O.V.
Experimental research of shaft sealing with elastic element made of MR material
Zhizhkin A.M., Zrelov V.A., Zrelov V.V.
Electronic model of turbine drive flow for its direct optimization
1 1.
Some issues of research and development in aviation industry
Korchak V.Y., Kuznetsov V.V., Borisenkov I.L., Leonovich G.I., Lukachev S.V., Biryuk V.V.
Key focus areas of samara state aerospace university research and education center of gasdynamic research
Matveev V.N., Anisimov M.Y.
Technical solutions of NOx decrease in traditional combustion chamber of GTE NK-16ST
Markushin A.N., Merkushin V.K., Byshin V.M., Baklanov A.V.
Influence of the burner form on the combustion chamber outlet temperature field ripple for different modes of operation of gas turbine engines
Markushin A.N., Baklanov A.V.
Cycled pressure of the multilayered multispan packagrcorrugated package
Eskin I.D., Alkeev R.I., Ivashchenko V.I.
Uniform and equidistant ways of structured computation grigd creation for CFD problems
Yefimow A.N., Matveev V.N.
Investigation of the gas turbine engine combustion chamber workflow
Markushin A.N., Baklanov A.V.
Method of reducing design aerodynamic characteristics to the results of drain tests of a transport category aircraft model
Bondar Y.I.
Test rig for a hydraulic drive under switched inertance control
Shorin V.P., Sverbilov V.Y., Gimadiev A.G., Greshniakov P.I., Ilyukhin V.N., Stadnik D.M.
1 - 23 of 23 Items

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