1. The concept of selecting the main parameters of a lightweight airplane with regard to the requirements of the contemporary Russian market

   • V. Yu. Demin
   • S. A. Yurgenson

   Flight Vehicle Design 26 August 2012 Pages: 113 - 119

2. Development of the weight formula for a folding wing

   • M. V. Yarygina
   • Yu. I. Popov

   Flight Vehicle Design 26 August 2012 Pages: 120 - 126

3. Formalization of solving the thermoelasticity problems for aircraft structures

   • A. S. Kretov
   • Wang Zhijin

   Structural Mechanics and Strength of Flight Vehicles 26 August 2012 Pages: 127 - 135

4. Approximate technique of tip vortex account in calculating a helicopter main rotor

   • A. Yu. Liss

   Structural Mechanics and Strength of Flight Vehicles 26 August 2012 Pages: 136 - 143

5. Calculation of flight vehicle main support wheel vibrations taking into account brake forces

   • V. S. Metrikin
   • M. A. Peisel’

   Structural Mechanics and Strength of Flight Vehicles 26 August 2012 Pages: 144 - 150

6. Contemporary approach to the design-systematic and experimental provision of autorotation landing safety for a helicopter with skid type landing gear

   • S. A. Mikhailov
   • D. V. Nedel’ko

   Structural Mechanics and Strength of Flight Vehicles 26 August 2012 Pages: 151 - 157

7. Wavelet filtering of measurement information in unmanned aerial vehicle control system

   • L. Yu. Emaletdinova
   • S. A. Lyasheva
   • M. P. Shleimovich

   Flight Dynamics and Control of Flight Vehicles 26 August 2012 Pages: 158 - 163

8. Statistical analysis for rotational motion of a light descent capsule under deployment of a space cable system

   • O. N. Naumov

   Flight Dynamics and Control of Flight Vehicles 26 August 2012 Pages: 164 - 169

9. Experimental studies of free flow boundaries influence upon aerodynamic characteristics of the clean large-scale models

   • V. V. Zherekhov
   • O. A. Ledyankina

   Aero- and Gas-Dynamics of Flight Vehicles and Their Engines 26 August 2012 Pages: 170 - 178

10. Calculation and experimental investigation of mixture formation in a vortex mixer

    • Sh. A. Piralishvili
    • R. I. Ivanov

    Aircraft and Rocket Engine Theory 26 August 2012 Pages: 179 - 183

11. A starting system of warning the critical conditions for a single-rotor helicopter

    • V. M. Soldatkin
    • A. A. Arkhipov
    • A. A. Uglov

    Aircraft Instruments and Instrumentation Computer Complexes 26 August 2012 Pages: 184 - 191

12. Theoretical determination of shot peening process parameters

    • Yu. P. Kataev

    Aircraft Production Technology 26 August 2012 Pages: 192 - 195

13. An engineering technique for evaluating the highly-porous cellular material geometry

    • Yu. A. Kirsanov
    • E. I. Ivanova

    Aircraft Production Technology 26 August 2012 Pages: 196 - 198

14. Development of control system algorithms for mini unmanned aerial vehicle of combined scheme — convertiplane

    • E. K. Syzdykov
    • A. V. Gainutdinova
    • K. G. Krikun

    Technical Notes Flight Vehicle Design 26 August 2012 Pages: 199 - 202

15. Assessment of GTE parts precision at the ion-plasma spraying of coatings

    • V. V. Budilov
    • R. M. Kireev
    • I. I. Yagafarov

    Aircraft Production Technology 26 August 2012 Pages: 203 - 207

16. Comparative analysis of mixing chambers for two multiphase flows of oppositely charged particles

    • M. P. Danilaev
    • S. A. Mikhailov
    • K. V. Faizullin

    Aircraft Production Technology 26 August 2012 Pages: 208 - 211

17. Optimization of CNC machine multitool operating regimes

    • E. M. Korovin
    • R. Kh. Valiev

    Aircraft Production Technology 26 August 2012 Pages: 212 - 216

18. Research and development version of computer-aided system of aircraft and rocket-space equipment vibration tests

    • V. A. Komkov
    • V. V. Vasilevskii
    • Yu. V. Mozgovoi

    Automation of Design and Production of Aeronautical Equipment 26 August 2012 Pages: 217 - 222