Participation in the international Projects Department of Aeromechanics and Flight Engineering Moscow Institute of Physics and Technology (State University)

First steps 2

Our partners 3

INTAS and ISTC Projects INTAS/AI Projects #632 External flow turbulence scale and level effect on aircraft wake characteristics at low speeds #1817 Experimental and Theoretical Investigation of Ion/Molecular Clusters in the Subsonic Turbulent Flow #1815 Development of Vortex Wake Visualization/Detection Methods Via Radiation and Scattering Fields Sensing #1816 Theoretical investigations of the influence of the aircraft engine jet on the wake vortex formation ISTC Partner’s Project with DFS Deutsche Flugsicherung GmbH #2086-p Wake turbulence problem in Frankfurt am Main airport final approach area

Vortex Safety. Problem statement Loaded airport with landscape 5 Il-114 on a glide path behind В-747, at a distance 5 km, calm atmosphere Near ground atmospheric boundary layer model Mountain landscape, high buildings and constructions Wind vortex wakes behind the obstacles+ induced (orographic) turbulence Aircraft during taxing, take-off and landing Flight simulator ANN Visualization of vortex wakes and turbulent zones Vortex wake behind the leading aircraft

MIPT as integrator of Russian Research Centers #0632#1816#1817#1815 FRI: Processing and postprocessing of the old WV Flight tests AI: A330/340 Experiments of K. Huenecke MATU: Unified approach to near and far aircraft vortex wake modeling by the discrete vortices method with taking into account unsteady effects MIPT, TsAGI: Experiments in two WT (preparatory stage) TsAGI, MIPT : Jet- Vortex Wake model CC: High-accuracy numerical methods for laminar and turbulent flows simulation MIPT: Physical models of visualization (ionization) FRI, TsAGI: Model of the atmosphere TASTC : Calculation of the viscous near wake behind the high-lift wing TsAGI: LES modeling Flow-field TsAGI, MIPT: Substantiation of the possibility of utilizing the thermal imager for WV detecting TsAGI, IAP: Substantiation of the possibility of utilizing the radio- frequency region for WV detecting NIIAO: Development of the conception of the onboard and ground-based lidar systems for WV detecting Turbulent background GPI: MM radio wave scattering on the acoustic disturbances 6

FP7 Research, Technological Development and Demonstration Aircraft concepts minimizing large cut-outs and extending lattice barrel sections Fuselage test panel, test rig 7 EUROPEAN COMMISSION Advanced Lattice Structures for Composite Airframes ( )

Workshop in TU Delft Prof. Z. Gürdal

HEXAFLY-INT International Flight Experiments on Civil High-Speed Air Transport European Partners ESA-ESTECNetherlandsEuropean Space Agency – European Space Research and Technology Centre EADS-MBDAFranceMBDA-France EADS-IWFrance/GermanyEADS-Innovation Work EADS-ASTRIUMFrance/GermanyASTRIUM DLRGermanyDeutsches Zentrum für Luft- und Raumfahrt CIRAItalyCentro Italiano Ricerche Aerospaziali ONERAFranceOffice National d'Etudes et de Recherches Aérospatiales GDLUKGas Dynamics Limited DEIMOSSpain USTUTTGermanyUniv. of Stuttgart Russian Partners TsAGIRussiaCentral Aerohydrodynamic Institute CIAMRussiaCentral Institute of Aviation Motors FRIRussiaFlight Research Institute MIPTRussiaMoscow Institute of Physics and Technology (State University) 9

HEXAFLY-INT High-Speed Experimental Fly Vehicles - INTernational Japanese Partners JAXAJapan MHIJapan IHIJapan Australian Partners UQAustraliaUniv. of Queensland UoSAustraliaUniv. of Sydney International Flight Experiments on Civil High-Speed Air Transport

Conclusions 1.MIPT has the experience as integrator of Russian Institutions participating in multidisciplinary projects 2.Joint research is working form of cooperation and very useful in education process 3.Possible research topics: Nondestructive testing (including equipment and mathematical simulation) Composite materials (including airworthiness norms, aging and resource) Flight safety and flight simulators of difficult flight regimes (atmospheric turbulence and human factor) Robotic systems and UAV (autopilots, optical vision, UAV in town canyon and safety…) Multidisciplinary optimization and Quick aerodynamic design at the stage of preliminary projection) 11

12 Contact Information Moscow Institute of Physics and Technology (State University) 9, Institutsky Per., Dolgoprudny Moscow Region Russian Federation Rector: Nikolay Kudryavtsev Phone: +7(495) Fax. +7(495) International Department Phone/Fax: +7(495) Department of Aeromechanics and Flight Engineering 16, Gagarin Str., Zhukovsky Moscow Region Russian Federation Dean: Victor Vyshinsky Phone: +7(495) Fax. +7(495) Prof. Victor V. Vyshinsky

Thank you for attention!!!