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Analysis of contact interaction of polymer honeycomb core and CFRP base layers in sandwich-core constructions
Pavlova S.A.
Mathematical modeling of interaction a high-frequency torch discharge with construction elements of radio equipment
Kostin A.V., Piganov M.N., Stolbikov A.V.
Fracture resistance criteria implementation while securing reliability of airplanes structural components during design stage
Tarasov Y.L.
Hemispherical high-speed particle transducer
Izyumov M.V., Syomkin N.D.
Optimization of honeycomb sandwich floor panels made of polymer-matrix low-combustible composite materials based on high-strength carbon and glass fibers and adhesive binder
Komarov V.A., Kutsevich K.E., Pavlova S.A., Tyumeneva T.Y.
Analysis of temperature fields of aircraft components
Azarenkov V.I.
Increasing the equivalence of realize full scale tests with the influence of geometrics parameters of the load system
Kulikov E.N.
Plane high-speed particle transducer
Izyumov M.V., Syomkin N.D.
Research of the possibility of thermal conditions LREST using an infrared thermal imaging system
Ryzhkov V.V., Silyutin M.V.
Testing of gas turbine engine bearing oil supply through an oil-catch ring
Boev A.A., Petrukhin A.G., Mikhailov A.A.
Design of reinforced specified fatigue life capability airframe panels containing notches
Bespalov V.A.
Laser vibrating method of gluing shells defects detecting
1 1., 1 1., 1 1., 1 1., 1 1.
Research and optimization of the choice sound-absorbing structures
Postnov V.I., Vyakin V.N., Veshkin E.A.
Dynamic behaviour of high- bypass- ratio turbofan carbon fiber-reinforced plastic blade ubder unsteady airloads
Buyukli T.V., Fedorchenko Y.P., Shorstov V.A.
Experimental verification of the specified characteristics of a solar battery at the stages of production and ground operation
Shuplyak Y.P., Sorokoletov V.I.
Analysis of the error of non-linearity of positional characteristics of a displacement transducer on multicomponent optronic structures
Matyunin S.A., Stepanov M.V.
Influence of the geometry fidelity of resonant sound-absorbing liner samples on their acoustic characteristics
Kustov O.Y., Khramtsov I.V., Bulbovich R.V.
Optimization of fatique validation cost for redesigned transport aircraft
Kleptsov V.I.
Research of influence of the thermal stream from the mid-flight liquid rocket engine on parameters of operating liquid rocket engines of small draught in the conditions of perspective razgonnogo's propulsion system of the block
Ageenko Y.I., Galperin R.N., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.
Developing a mathematical model of aircraft honeycomb sandwiches
Tits S.N.
Construction of limitation diagrams for truss core stiffness and strength parameters
Gainutdinov V.G., Gainutdinova T.Y., Abdullin I.N.
Laser measurement systems for structural elements’ spacing check
Mordasov V.I., Sazonnikova N.A., Nonin A.S.
System design of follow shearing dies for cutting sheet blank
Pochekuev E.N., Skripachev A.V., Shenberger P.N.
The main trends of aviation science development
Alyoshin B.S., Chernyshev S.L.
Determination of large-size liner impedance based on numerical simulation of sound propagation in a duct with specified azimuthal modal structure
Korin I.A., Palchikovskiy V.V., Pavlogradskiy V.V.
Optimization of the design of a railway searchlight in the ANSYS software environment
Abulkhanov S.R.
Experimental definition of the optimum scheme of shaping forged impellers by high-speed forging
Khaimovich A.I.
Assuring the durability of transport aircraft structure in multipurpose use based on the results of endurance and flight tests
Fomichev P.A., Kleptsov V.I.
Optimal design of sandwich floor panels made of high-strength composite materials considering stiffness constraints
Komarov V.A., Pavlova S.A.
Сhoice of materials for producing dimensionally stable load-carrying structures
Bitkin V.E., Zhidkova O.G., Komarov V.A.
Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel
Ageenko Y.I., Lapshin E.A., Morozov I.I., Pegin I.V., Ryzhkov V.V.
System for assessing the consistency of radioelectronic device design and the manufacturer’s technology at the stage of mastering
1 1.
Choosing the place for the installation of navigation system aerials on the ERS spacecraft body
Akhmetov R.N., Kurenkov V.I., Stratilatov N.R., Shilov L.B., Gordeev A.I.
1 - 33 of 33 Items

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