Computer-aided formation of the aircraft appearance on the basis of base version reconfiguration N. A. EreminN. K. Liseitsev Flight Vehicle Design 03 February 2010 Pages: 377 - 382
Analysis of shells of revolution under symmetrical loading using the quadrature method I. S. Akhmed’yanov Structural Mechanics and Strength of Flight Vehicles 03 February 2010 Pages: 383 - 389
Investigation of direct integration for nonlinear finite element equations of motion by the modified central difference method N. A. KaluginL. M. Savel’ev Structural Mechanics and Strength of Flight Vehicles 03 February 2010 Pages: 390 - 393
A technique for predicting strength properties of an aircraft wing V. V. KashkovskiiI. I. TikhiiS. P. Poluektov Structural Mechanics and Strength of Flight Vehicles 03 February 2010 Pages: 394 - 398
Analysis of chaotic vibrations for the distributed systems in the form of the Bernoulli-Euler beams using the wavelet transform A. V. Krys’koM. V. ZhigalovV. V. Soldatov Structural Mechanics and Strength of Flight Vehicles 03 February 2010 Pages: 399 - 407
A method for constructing an airfoil using a specified chord velocity diagram R. B. SalimovA. G. Labutkin Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 03 February 2010 Pages: 408 - 412
Statistical analysis of experimental study results on low-cycle fatigue resistance for the EI698-VD high-temperature alloy N. P. Velikanova Aircraft and Rocket Engine Design and Development 03 February 2010 Pages: 413 - 418
Choice of flight conditions and modes of engine operation for its diagnostics D. A. IonovV. B. Korotkov Aircraft and Rocket Engine Design and Development 03 February 2010 Pages: 419 - 425
Dynamics of a rigid rotor in the NK-14ST-10 engine free power turbine with sliding bearings K. N. ChaadaevD. K. Novikov Aircraft and Rocket Engine Design and Development 03 February 2010 Pages: 426 - 431
Providing the maximum cycle work as a promising direction in development of gas turbine plants V. A. Ivanov Aircraft and Rocket Engine Theory 03 February 2010 Pages: 432 - 439
Stochastic calculation of the flowrate distribution along the cooling path channels in the liquid rocket engine chamber A. V. KretininYu. A. BulyginP. A. Dronov Aircraft and Rocket Engine Theory 03 February 2010 Pages: 440 - 443
A technique for formation and application of informative failure danger functions in the integrated airborne equipment complex N. N. MakarovV. M. Soldatkin Aircraft Instruments and Instrumentation Computer Complexes 03 February 2010 Pages: 444 - 454
Aerometric system for measuring low helicopter airspeeds based on the data of the vortex column position V. V. Soldatkin Aircraft Instruments and Instrumentation Computer Complexes 03 February 2010 Pages: 455 - 462
Special features of a digital speckle interferometer for determining vibration characteristics of heavy-loaded elements of an aircraft fuel pump O. A. ZhuravlevE. V. ShakhmatovA. I. Dolgov Aircraft Production Technology 03 February 2010 Pages: 463 - 467
Diagnostics of GTE turbine blades using a new vibroacoustic method I. V. Ivshin Aircraft Production Technology 03 February 2010 Pages: 468 - 473
Tensor representation of the aircraft hydraulic system structure M. A. Kovalev Automation of Design and Production of Aeronautical Equipment 03 February 2010 Pages: 474 - 479
Modeling stress strain state of thin shells with a degenerating domain F. S. Khairullin Technical Notes Structural Mechanics and Strength of Flight Vehicles 03 February 2010 Pages: 480 - 483
Simulation of a flexible spacecraft motion to evaluate microaccelerations A. V. Sedel’nikovA. A. Serpukhova Flight Dynamics and Control of Flight Vehicles 03 February 2010 Pages: 484 - 487
Influence of fuel hydrogen additives on the characteristics of a gas-piston engine under changes of an ignition advance angle Yu. F. GortyshovV. M. GureevA. P. Shaikin Aircraft and Rocket Engine Design and Development 03 February 2010 Pages: 488 - 490
Device for plate metal laser cutting V. N. AnaninYu. P. Kataev Aircraft Production Technology 03 February 2010 Pages: 491 - 494