Nonlinear bending and stability of circular plates under the liquid pressure and temperature M. S. GaneevaV. E. MoiseevaZ. V. Skvortsova Structural Mechanics and Strength of Flight Vehicles 06 July 2016 Pages: 1 - 7
Development of the discrete vortex cylinders method for calculating the helicopter rotor induced velocity E. I. NikolaevM. N. Nikolaeva Structural Mechanics and Strength of Flight Vehicles 06 July 2016 Pages: 8 - 14
Analytical construction of interception trajectories in atmosphere V. A. Afanas’evG. L. DegtyarevA. S. Meshchanov Flight Dynamics and Control of Flight Vehicles 06 July 2016 Pages: 15 - 22
Space vehicle landing dynamics at failure of landing gear V. N. BakulinS. V. BorzykhV. V. Voronin Flight Dynamics and Control of Flight Vehicles 06 July 2016 Pages: 23 - 28
Stability of the stationary motion of the airship V. T. Grumondz Flight Dynamics and Control of Flight Vehicles 06 July 2016 Pages: 29 - 35
Studies of the screening surface proximity on integral aerodynamic characteristics of rectangular high-lift wings of different aspect ratio K. V. BukanovV. V. Zherekhov Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 06 July 2016 Pages: 36 - 43
Computational modeling of interference between helicopter main and tail rotors based on nonlinear blade vortex model Yu. M. IgnatkinP. V. MakeevA. I. Shomov Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 06 July 2016 Pages: 44 - 50
Weight optimization principles for turbine blade shroud platform A. I. BelousovS. V. Nazdrachev Aircraft and Rocket Engine Design and Development 06 July 2016 Pages: 51 - 57
Development of the design scheme of cooling for a nozzle vane of high pressure turbine of gas turbine engine A. V. VikulinN. L. YaroslavtsevV. A. Chesnova Aircraft and Rocket Engine Design and Development 06 July 2016 Pages: 58 - 63
Calculation of design relative density for rational sandwich structure with truss core V. G. GainutdinovI. N. AbdullinS. M. Musavy-Safavy Aircraft and Rocket Engine Design and Development 06 July 2016 Pages: 64 - 68
Development, research and production of a centrifugal impeller V. M. GureevR. R. SalakhovV. V. Burlakov Aircraft and Rocket Engine Design and Development 06 July 2016 Pages: 69 - 76
Concept of monitoring for thermostressed state and service life of aircraft gas turbine engine blades G. G. KulikovV. A. TrushinA. A. Ganeev Aircraft and Rocket Engine Design and Development 06 July 2016 Pages: 77 - 83
Studies of GTE reverse jets distribution G. F. MingaleevS. G. MargulisA. V. Kosterin Aircraft and Rocket Engine Design and Development 06 July 2016 Pages: 84 - 88
Special features of aerodynamic and thermal improvement of turbine nozzles for advanced gas turbine engines V. A. PoletaevA. E. RemizovV. V. Lebedev Aircraft and Rocket Engine Design and Development 06 July 2016 Pages: 89 - 94
Pressure recovery in a planar diffuser at pulsatory flow regimes I. A. DavletshinN. I. MikheevA. A. Paerelii Aircraft and Rocket Engine Theory 06 July 2016 Pages: 95 - 99
Simulation of thermal radiation emitted by heterogeneous combustion products in the combustion chamber of a model engine V. A. Kuz’minE. I. MaratkanovaR. V. Rukavishnikova Aircraft and Rocket Engine Theory 06 July 2016 Pages: 100 - 106
A high-temperature frameless starter-generator integrated into an aircraft engine F. R. IsmagilovI. Kh. KhairullinV. I. Bekuzin Aircraft Instruments and Instrumentation Computer Complexes 06 July 2016 Pages: 107 - 111
Practice in the application of specialized technologic process patterns of 5-axis machining operation of blade rings of blisks I. N. KhaimovichO. S. SurkovA. I. Khaimovich Aircraft Production Technology 06 July 2016 Pages: 112 - 117
Peculiarities of the control actuator development on the basis of combined electromechanical modules V. V. MorozovA. V. Zhdanov Automation of Design and Production of Aeronautical Equipment 06 July 2016 Pages: 118 - 125
Strength design model for thin-walled structures Z. J. WangL. H. KangS. Huang Technical Notes/Structural Mechanics and Strength of Flight Vehicles 06 July 2016 Pages: 126 - 133
Analysis of stress state in a root-airfoil transition zone of hollow wide chord fan blades V. K. BerdinA. M. SmyslovV. V. Luk’yanov Aircraft and Rocket Engine Design and Development 06 July 2016 Pages: 134 - 137
Numerical simulation of the flow in the rotation cavities of turbopump assembly D. A. ZhuikovV. P. Nazarov Aircraft and Rocket Engine Theory 06 July 2016 Pages: 138 - 144
Statistical analysis of stretch shaping process of biconvex skin V. A. MikheevS. D. Smol’nikovD. V. Savin Aircraft Production Technology 06 July 2016 Pages: 145 - 150
An investigation of electrical conductivity of aluminum alloy semi-finished products used in aircraft manufacture V. V. SemenychevR. K. Salakhova Aircraft Production Technology 06 July 2016 Pages: 151 - 155
