No. 2, 2009
- Факультету летательных аппаратов военно-воздушной инженерной академии имени профессора н.е. жуковского 85 лет pp. 5
- Analysis of Flight Characteristics and Estimation of Combat Possibilities of the Fifth-Generation Fighter F-22A «Raptor pp. 10
- Analysis of Flight Characteristics and Estimation of Combat Possibilities of the Fifth-Generation Fighter Bomber F-35 pp. 19
- Substantiation of Criteria for the Choice of Rational Engineering Solutions at the Design of a Fighter Aircraft pp. 26
- Method of Desigh of Motion of Airplane on the Zakriticheskikh Corners of Attack pp. 33
- The Aircraft-s Elements with the Control Surfaces Aeroelasticity Characteristics in the Separate Flow Research pp. 38
- The Tandem-Type Wings Aerodynamic Characteristics in the Separate Flow Research pp. 43
- The Possibility of the Discrete Vortexes Method Improved Quadrature Formulae Use in the Aeroelasticity Problems pp. 46
- Approach to Method of Calculating the Yield of Dispersed Carbon in Methane-Oxygen Gas Generator of Jet Engine pp. 52
- Studies of Oxidation Processes in Fuels for Aircraft Gas Turbine Engines in Conditions of Two-Phase Closed System pp. 56
- Method for Evalvation of Corrosion Activity of Jet Fuel at Increased Temperatures pp. 62
- The Study of Protective Aluminum Coating Layers pp. 65
- Modernisation of device IVR-1 pp. 68
- Energy-Saving Technology of the Burns Control of Titanium Compressor Blade of Gas Turbine Engine on Fluctuation of Work Function pp. 73
- Computerizing the «Descriptive Geometry. Engineering Graphic Arts» Discipline pp. 77
- Prediction of Manouever Aircraft Movement It the Problem of Improoving Pilot-s Overload Protection pp. 82
- Structural Changes Evaluation of Turbine Disks Geometry for Stress Concentration Zone pp. 89
- The Knowledge Role in the Management of the Innovation Process in Holding Companies pp. 94