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Research of technological heredity influence on setting of procedure of measurements on coordinate-measurement machine in case of out-of-flatness detecting for aircraft engineering parts
Cheveleva A.O., Bolotov M.A.
Methods of validation of the ballistic structure of space surveillance system orbital segment
Fadin I.A., Yanov S.V., Samokhvalov O.A.
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.
On a method of practical training fulfillment for course of studies “Design of Main Units and Systems of Engine”
Borisov V.A., Zhizhkin A.M.
Designing a seal as an element of air secondary system in aircraft engines
Vinogradov A.S.
Unit impulse input tests of a system of the «Frigate» upper-stage rocket
Mikhalenkov N.A., Yermakov V.Y., Utkina Y.I.
Aspects of the numerical method calculating thermogazodynamic lrest based on not perfect passing of workflows in the combustion chamber
Silyutin M.V., Shustov S.A.
Development of a single-section demonstrator rotary engine on the basis of a modern complex design procedure
Kostyuchenkov A.N., Zelentsov A.A., Semenov P.V., Minin V.P.
Dimensions of controlled on CMM flat surfaces as an influencing factor of their coordinate-positional parameters measurement errors
Cheveleva A.O., Bolotov M.A.
Experimental determination of acoustic loads daunches of Strela LV and calculation of test modes for a spacecraft to be delivered by it to space
1 1., 1 1., 1 1., 1 1.
Method of calculation and analysis of gas flow aerodynamic indices in a vortex wind power plant
Biryuk V.V., Uglanov D.A., Gorshkalev A.A., Bolshov D.V., Krasnorutskiy A.S., Lapshina V.A., Chertykovtsev P.A.
Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants
Silyutin M.V., Shustov S.A.
Designing of low-flow rate slider bearings for turbomachinery rotors
Parovay E.F.
Measuring system for investigation flow rate and fluid pressure features of control devices for the position hydrodrive
Poleshkin M.S., Sidorenko V.S.
Assessment of technicaland economical efficiency of developing carrier rockets with first-stage reusable units
1 1., 1 1.
Internal combustion engine some cooling system components detailed calculation
Kolomin I.V., Ajukov A.A., Birjuk V.V.
Analysis of the thermal state of aircraft engine supports
Vinogradov A.S., Badykov R.R., Fedorchenko D.G.
Finite element techniques for pipe system vibroacoustical characteristics modelling
Mironova T.B., Prokofiev A.B., Shorin V.P.
Development of the design procedure of the shaping rigging with the use of the integrated information systems
, ,
Measurment procedure optimizing geometrical parameters of measure GTE feature on coordinate measuring machine
Bolotov M.A., Cheveleva A.O., Zhidyaev A.N.
Methods of organization and evaluation of the results of planning economic activity of industrial enterprises based on IPF-technologies
Khaytbaev V.A., Nemchinov O.A.
Methodology of analysis temperature stresses in chips
Krasnoschekova G.F., Tyulevin S.V., Nasedkin A.V., Mishanov R.O.
Working out of methods preporation of execution technological audit for rearmament innovation factory
, ,
Numerical simulation of low liquid flow in a mixer consisting of two centrifugal swirlers
Semkin E.V.
Methods and the experiment of the parametric identification compressors and fans mathematical models of according to the results of the gas turbine engine development test
Kofman V.M.
Method of calculating of the load characteristics of cylindrical support with a discrete location of elastic damping elements of the MR material
1 1., 1 1., 1 1., 1 1., 1 1.
Technique of compensating errors in machining of parts with sculptured surfaces
Pechenin V.A.
Procedure of calculating efforts of blank stretching without corrugation in stretch forming
Dementyev S.G.
Models and methods of optimizing the procedure of measuring gas turbine engine parts using coordinate measuring devices
Bolotov M.A., Lyozin I.A.
Decrease in toxicity of transport diesel engines by neutralisation nitrogen oxide of the fulfilled gases
1 q., 1 1.
Comparative estimation of the accuracy of methods of autonomous navigation of small spacecraft in formation flying
Golyakov A.D., Richnyak A.M., Kalabin P.V.
Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks
Gimadiev A.G., Sverbilov V.Y., Stadnik D.M.
A simplified method of thermoacoustic engine analysis
Zynovyev E.A., Dovgyallo A.I.
Research of errors of measuring angular location parameters of holes in turbine and compressor discs of gas turbine engines
Bolotov M.A., Zhidyaev A.N., Shitarev I.L., Cheveleva A.O.
Analysis of temperature separation efficiency in vortex gas flows
Biryuk V.V., Kurnosov N.Y., Tarnopolsky A.V.
1 - 35 of 35 Items

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