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Research of radial face contact seal tightness in the support of the aircraft engine compressor at various operational modes
Vinogradov A.S., Badykov R.R., Shpakov I.D.
Characteristics of metal rubber material for large short-term loading
Ulanov A.M., Ponomarev Y.K., Parovay F.V.
Three-dimensional inhomogeneous thermal fields of the “Photon-Amur 2.0” payload electronic board developed for nanosatellites
Fomin D.V., Barulinа M.A., Golikov A.V., Strukov D.O., German A.S., Ogorodnikov A.A.
Assessing the efficiency of flights to high near-earth orbits using boosters with chemical and electro-rocket engines
Ishkov S.A., Fadeenkov P.V., Balakin V.L.
Forces distribution in thread and external altering load factor in thread joint under structures vibration
Kurushin M.I., Kurushin A.M., Barmanov I.S.
Thin-walled plates and covers with surface-crack defects in elastoplastic approach
Astafiev V.I., Yakovlev A.S.
Investigatiom of interrelation of gluing designs defects from polymeric composite materials
Mordasov V.I., Storozh A.D., Grebnev N.E., Grebnev D.N., Shulepova O.V.
Automated generation of structural members of a spacecraft thermal model
Kulikov D.S., Shatin A.A., Velmisov I.G.
Thermal design of «AIST» small spacecraft
Kulikov D.S., Erilkin J.N.
Optimization of thermomechanical parameters of high speed forging of titanium alloys
Khaimovich A.I., Mikheyev V.A.
The influence of residual technological stress and service heat loads on the strength of railway wheels
Kerentcev D.E., Ponomarev J.K.
Complex approach to mechanical tests of executive automatic units of space vehicles
1 1., 1 1., 1 1.
Dynamic behaviour of high- bypass- ratio turbofan carbon fiber-reinforced plastic blade ubder unsteady airloads
Buyukli T.V., Fedorchenko Y.P., Shorstov V.A.
The determination of various factors influencing on change of the mounting fit and calculation procedure of the load distribution in the cylindrical roller bearings operated in tightness
1 1.
Assessing the impact of non-through cracks (scratches) on the structural strength when designing aircraft
Yakovlev A.S.
Calculation of the double-row spherical roller bearing of the satellite gear wheel of the planetary reducer
Zhilnikov E.P., Murashkin V.V., Shifrin I.M.
1 - 16 of 16 Items

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