Mathematical model of balancing for a vertical takeoff and landing disk-wing aircraft A. M. GirfanovV. V. Pavlov Flight Vehicle Design 23 May 2010 Pages: 1 - 8
Simulation of elastoplastic deformation of helicopter skid landing gear springs S. A. MikhailovL. V. KorotkovD. V. Nedel’ko Structural Mechanics and Strength of Flight Vehicles 23 May 2010 Pages: 9 - 15
Fatigue life of a plate with an arbitrary-shaped concentrator under low-cycle plane loading A. T. PonomarevV. G. StopkevichE. V. Korobeinikov Structural Mechanics and Strength of Flight Vehicles 23 May 2010 Pages: 16 - 25
Mathematical modeling of an optimal controlled helicopter flight at vertical regimes A. G. AuzyakV. I. BudinF. V. Dremov Flight Dynamics and Control of Flight Vehicles 23 May 2010 Pages: 26 - 32
An efficient method for determining a distance at direction finding of target with partially-known parameters Yu. G. BulychevA. A. Mozol’V. N. Vernigora Flight Dynamics and Control of Flight Vehicles 23 May 2010 Pages: 33 - 38
A method for determining velocities and accelerations of an elastic main rotor blade element V. A. Leont’ev Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 23 May 2010 Pages: 39 - 44
Influence of the open end geometry on resonance oscillations of a gas in a tube L. A. TkachenkoR. G. Galiullin Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 23 May 2010 Pages: 45 - 50
Choice of support arrangement in designing two-support rotors of gas turbine engines V. A. ZrelovA. S. MironovM. E. Prodanov Aircraft and Rocket Engine Design and Development 23 May 2010 Pages: 51 - 56
A technique for presentation and application of the propeller fan multidimensional characteristics in semi-full-scale simulation of a gas turbine engine and its automatic control system I. A. KrivosheevA. G. GodovanyukG. I. Pogorelov Aircraft and Rocket Engine Design and Development 23 May 2010 Pages: 57 - 62
Improvement of conventional combustion chamber structure in order to enhance GTE ecological indicators A. N. MarkushinV. K. MerkushinA. V. Baklanov Aircraft and Rocket Engine Design and Development 23 May 2010 Pages: 63 - 68
Investigation of power gas turbine drives on the basis of mathematical models B. M. OsipovA. V. TitovA. R. Khammatov Aircraft and Rocket Engine Design and Development 23 May 2010 Pages: 69 - 72
Calculation of energy parameters in high-speed centrifugal pumps of low specific speed E. M. Kraeva Aircraft and Rocket Engine Theory 23 May 2010 Pages: 73 - 76
Flight efficiency of a pulsejet V. N. Pobezhimov Aircraft and Rocket Engine Theory 23 May 2010 Pages: 77 - 80
Mathematical modeling and experimental investigations of oxygen-methane fuel combustion at coaxial-jet supply into the combustion chamber of liquid-propellant rocket engine V. R. RubinskiiS. P. KhrisanfovA. V. Kretinin Aircraft and Rocket Engine Theory 23 May 2010 Pages: 81 - 86
A method for calculating the laser rocket engine thermal state based on the optical discharge with numerous plasma formations A. G. Sattarov Aircraft and Rocket Engine Theory 23 May 2010 Pages: 87 - 94
Intensification of heat exchange on the convex surface of an annular channel with continuous flow swirling A. V. ShchukinA. V. Il’inkovN. F. Maksimov Aircraft and Rocket Engine Theory 23 May 2010 Pages: 95 - 101
Analysis of shells of revolution under reversely symmetrical loading using the quadrature method I. S. Akhmed’yanov Technical Notes 23 May 2010 Pages: 102 - 107
Application of the Abel equation to describe the precession motion of a gyrostabilized platform V. A. PogorelovT. V. KlodinaA. I. Sapozhnikov Flight Dynamics and Control of Flight Vehicles 23 May 2010 Pages: 108 - 112
Application of oil dispersion to enhance the efficiency of aircraft GTE oil system operation V. N. Pon’kinB. A. Kessel’V. V. Takmovtsev Aircraft and Rocket Engine Design and Development 23 May 2010 Pages: 113 - 116
Thermodynamic properties of mixed fuel combustion products A. B. ShigapovI. Yu. SilovA. A. Shigapov Conversion of Aeronautical Equipment and Production 23 May 2010 Pages: 117 - 119
