2008, vol. 15, no. 5

Aircraft Engineering
	Ovchinnikov S. Y. Operation features of double-chamber shock-stuts with two kinds of structure
	Vinepres A. L. Flight simulator evaluation of piloting process for a single-rotor helicopter with fly-be-wire backup control system using side control levers
	Abashev O. V., Kuprikov M. Y. An application of artificial neural networks in aircraft design
Propulsion and Power Plants
	Stepanenko S. A. Gas dynamics and interphase heat exchange foe supersonic heterogeneous flow inleaking on some obstacle
	Abgarian V. K., Ryzhov Y. A. A predictive model of erosion calculation for ion-plasma sources and discharge chamber channel walls in stationary plasma engine
	Avrashkov V. N., Metelkina E. S., Meshcheriakov D. V. Flame air heater for wide-range scramjet combustor research
	Krylov B. A., Onishchik I. I., Yun A. A. A calculation of temperature fields for a model of mixing combustion chamber
Engineering
	Nikitin P. V., Stepanenko S. A. A technique for assessment of blackness level for heat resistant coatibgs
Computer Science and Control
	Baranov V. N., Li B. K. Optimal control of light airplane during flight tests
	Malyshev V. V., Li W., Baranov V. N. A technique of correlation analysis for characteristics of instrumentation used to support flight tests of light airplanes
Economics
	Sorokin A. E., Shcherbakova E. A. A technique to evaluate financial and economical condition of aircraft industry enterprises
Applied Mathematics, Mechanics and Physics
	Gidaspov V. Y., Pirumov U. G., Severina N. S. Mathematical modeling of quasi-one-dimensional non-steady flows of reacting gas with arbitrary number of interacting discontinuities
	Shtyrlin A. F. Focusing properties of a single emission cell for colloid electrojet engine
	Vinnikov V. V., Reviznikov D. L., Sposobin A. V. An estimation of influence zone for electric field generated with overhead power transmission line
	Alifanov O. M., Cherepanov V. V. Identification of physical properties for highly porous fibrous material by means of statistical modeling techniques
	Golovanov A. I., Mitryaikin V. I., Shuvalov V. A. An investigation of stess-strain state for hingeless torsion bar of helicopter rotor in geometrically nonlinear statement
	Orlov V. N. About a teachnique to solve approximately matrix differential Riccati equations
	Belitsyn I. V., Kotyrlo T. V., Spirin G. G. An estimation of influence zone for electric field generated with overhead power transmission line

mai.ru — informational site of MAI

2008, vol. 15, no. 5

Aircraft Engineering

Propulsion and Power Plants

Engineering

Computer Science and Control

Economics

Applied Mathematics, Mechanics and Physics