Calculation of heat conduction in aerospace plane thermal protection system Zhijin WangHong YeA. S. Kretov Flight Vehicle Design 18 December 2013 Pages: 213 - 218
Dynamics of a cylindrical shell with a locally damaged protective coating B. A. Antuf’ev Structural Mechanics and Strength of Flight Vehicles 18 December 2013 Pages: 219 - 223
Modeling of helicopter behavior dynamics under the controlling action of the stabilization and control system E. V. Kasumov Structural Mechanics and Strength of Flight Vehicles 18 December 2013 Pages: 224 - 228
Thermoelastic problem for a physically orthotropic cylindrical shell at localized temperature B. V. NerubailoVu Ba Zui Structural Mechanics and Strength of Flight Vehicles 18 December 2013 Pages: 229 - 233
Theoretical and experimental technique of determining the mechanical characteristics of folded structure filler in the form of Z-crimp (shear of a filler in cross-sectional planes) V. N. PaimushinI. M. ZakirovYu. A. Karpikov Structural Mechanics and Strength of Flight Vehicles 18 December 2013 Pages: 234 - 246
Algorithms of constructing a neural network model for a dynamic object of control and adjustment of PID controller parameters L. Yu. EmaletdinovaE. D. Tsaregorodtseva Flight Dynamics and Control of Flight Vehicles 18 December 2013 Pages: 247 - 256
Application of neural networks for the design of flight control algorithms. II Adaptive tuning of neural network control law A. I. Kondrat’evYu. V. Tyumentsev Flight Dynamics and Control of Flight Vehicles 18 December 2013 Pages: 257 - 265
Analysis of nonstationary heating and cooling of a thermomagnetic engine gadolinium working element D. A. GabrielyanV. V. SemenovD. S. Martirosov Aircraft and Rocket Engine Design and Development 18 December 2013 Pages: 266 - 273
Computer-aided design analysis of hypersonic aircraft air intake geometry V. G. Gainutdinov Aircraft and Rocket Engine Design and Development 18 December 2013 Pages: 274 - 279
On synthesizing the informative functions of hazard at helicopter’s critical flight conditions O. I. KuznetsovV. M. Soldatkin Aircraft Instruments and Instrumentation Computer Complexes 18 December 2013 Pages: 280 - 290
System engineering design of a vortex aerodynamic angle and true airspeed sensor E. S. Soldatkina Aircraft Instruments and Instrumentation Computer Complexes 18 December 2013 Pages: 291 - 296
Probabilistic estimation of fulfilling favorable conditions to realize the gravity-sensitive processes aboard a space laboratory A. I. BelousovA. V. Sedel’nikov Technical Notes 18 December 2013 Pages: 297 - 302
Forced aeroelastic oscillations of a rotating anisotropic helicopter main rotor blade at hovering T. V. GrishaninaF. N. Shklyarchuk Structural Mechanics and Strength of Flight Vehicles 18 December 2013 Pages: 303 - 313
On influence of energy-producing additives upon the service characteristics of aviation fuels L. S. YanovskiiN. I. VarlamovaI. M. Popov Aircraft and Rocket Engine Design and Development 18 December 2013 Pages: 314 - 318