Temperature strain of a shallow cylindrical shell under local damage of a protective layer B. A. Antuf’ev Structural Mechanics and Strength of Flight Vehicles 06 May 2008 Pages: 1 - 4
Influence of element strength and stability on the behavior of SPRE igniter in critical situations A. A. KorenevF. A. Urazbakhtin Structural Mechanics and Strength of Flight Vehicles 06 May 2008 Pages: 5 - 10
Dependence of helicopter lifting system loading on temperature variations in composite material properties S. A. MikhailovA. M. GirfanovA. S. Fal’ko Structural Mechanics and Strength of Flight Vehicles 06 May 2008 Pages: 11 - 15
High-precision control of the observation satellite with small power consumption A. S. Meshchanov Flight Dynamics and Control of Flight Vehicles 06 May 2008 Pages: 16 - 25
Transmission of stress waves through the solid-gas media boundary Yu. P. KataevI. M. Zakirov Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 06 May 2008 Pages: 26 - 33
Simulation of the test stand gas-liquid ejector operation V. Ya. ModorskiiA. V. Kozlova Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 06 May 2008 Pages: 34 - 39
Nonlinear resonance gas oscillations in a flat open-ended channel A. V. RepinaR. G. Galiullin Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 06 May 2008 Pages: 40 - 46
Hardware-in-the-loop testing technology for integrated control and condition monitoring systems of aircraft gas turbine engines G. G. KulikovV. Yu. Ar’kovA. I. Abdulnagimov Aircraft and Rocket Engine Design and Development 06 May 2008 Pages: 47 - 52
Determination of natural frequencies and vibration modes of a constant thickness centrally secured disk R. Kh. MakaevaA. M. TsarevaA. Kh. Karimov Aircraft and Rocket Engine Design and Development 06 May 2008 Pages: 53 - 59
Operation algorithm synthesis for the information-control system of inspection and diagnostics of aircraft equipment state N. N. Makarov Aircraft Instruments and Instrumentation Computer Complexes 06 May 2008 Pages: 60 - 66
GTE gas temperature determination with the use of indirect measurements V. I. Petunin Aircraft Instruments and Instrumentation Computer Complexes 06 May 2008 Pages: 67 - 74
Dynamics of an ultrasonic impact tool with an intermediate striker M. M. Ganiev Aircraft Production Technology 06 May 2008 Pages: 75 - 83
A problem of choosing a generalized parameter of flexible spacecraft structures to construct a fractal model of microaccelerations A. V. Sedel’nikov Technical Notes 06 May 2008 Pages: 84 - 86
On estimation of total pressure internal losses in the axial-inlet annular diffuser channels E. N. BogomolovA. V. Kashcheev Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 06 May 2008 Pages: 87 - 89
Cooled two-stage GTE turbine with a tubular or tubular-annular combustion chamber R. S. AgachevV. A. SychenkovP. A. Stepanov Aircraft and Rocket Engine Design and Development 06 May 2008 Pages: 90 - 93
A probabilistic assessment of cycle life of GTE disks made of granular materials M. Sh. NikhamkinD. A. Vyatchanin Aircraft and Rocket Engine Design and Development 06 May 2008 Pages: 94 - 96
Special features of accelerated aerosol coagulation under subharmonic resonance in an open tube N. V. Sonin Aircraft and Rocket Engine Theory 06 May 2008 Pages: 97 - 100
Investigation of phase inhomogeneity of rhenium-bearing nickel alloy single crystals N. A. Protasova Aircraft Production Technology 06 May 2008 Pages: 101 - 104
Structure of technological-purpose automation models by the example of a computer-aided design system of labor standards I. Sh. Sharafeev Economical Aspects in Aircraft Engineering 06 May 2008 Pages: 105 - 108