Development of thermal protection systems for interplanetary flight.
Development of New Methods of Laminar Flow Control and Turbulent Drag Reduction.
Ecological Aspects of the Impact of a Supersonic Civil Aircraft (SST) of the Second Generation of Environment . Methods of Reducing Sonic Boom, Community Noise and the Supersonic Civil Aircraft Impact on the Ozone Layer.
Problems of Investigation of Aircraft Vortex Wake Evolution and Flight Safety.
#0548Flying Wing Airplane
Investigations of Technologies, Critical for Implementing an Airplane of Flying Wing Type with Superhigh Seating Capacity
Development of a Complex Technique for Testing Highly-Economical, Ecologically-Promising Civil Aircraft in Transonic Wind Tunnels
Multidisciplinary Approach to Preparing the Concept of Second-generation Supersonic Transport Airplane (SST-2) Ensuring Perfect Aerodynamic, High Static/Fatigue Strength, Good Structural Efficiency and Safe Flights
New Approaches to Predictive Joints Design Based on a Detailed Description of Local Elasto-Plastic Strain History by Combining the Holographic Interferometry Data and Numerical Simulation
Development of Methods for Calculating Shapes of Ice Formations and their Impact on Aerodynamic Characteristics, Stability, Control and Flight Safety of Civil Aircraft
Aerodynamics of Super and Hypersonic Vehicles
#1018Aircraft Vortex Wake
Flight Safety, Aircraft Vortex Wake and Airport Operation Capacity
New Dynamic Models of Unsteady Viscous Transonic Aerodynamics
Optimization of 3-D Components and Integrated Configurations of Supersonic Aircraft
Problems of Aerothermoballistics, Radiation Gasdynamics, Heat and Mass Transfer for Planet Sample Return Missions
Development of Airliners' Automation and Aircrew Information Principles to Enhance Flight Safety
Development of a Complex Technique for Testing Highly-Economical Civil Aircraft in Transonic Wind Tunnels with Slotted Walls
Theoretical and Numerical Investigations of Active/passive Concepts to Demonstrate the Impacts from Aeroelasticity on the Improvement of Aircraft Performance
Supersonic Civil Aircraft Impact on Environment
Development of a New Conception of the Efficient Industrial Mixer for Making High-Quality Suspensions and Emulsions
Investigation and Development of New Methods of Flow Control for Modern Passenger Aircraft Aerodynamics Improvement
New Approaches to Predictive Joints Design Based on Detailed Description of Local Elasto-Plastic Strain History by Combining the Holographic Interferometry Data and Numerical Simulation
Study of Wind-Tunnel Turbulence Influence on the Structure and Characteristics of Shear, Separated and Swirling Flows
Investigation of Steady and Unsteady Phenomena in Transonic Wind Tunnels with Slotted Walls to Improve a Complex Technique for Testing Highly-Economical Civil Aircrafts
Stress determination on a base of advanced interferometric measurements of deformation response induced by local mechanical influence
Analysis of Aircraft Aeroelasticity with Taking into Account Nonlinearities and Uncertainties
Comprehensive Study of Shock Wave Interference with a Turbulent Boundary Layer, High-Enthalpy Layer, and Vortex Structure
The Effect of Shock Waves Movement on Flutter and Self-Oscillations of an Elastic Aircraft in Transonic Flow
The International Science and Technology Center (ISTC) is an intergovernmental organization connecting scientists from Kazakhstan, Armenia, Tajikistan, Kyrgyzstan, and Georgia with their peers and research organizations in the EU, Japan, Republic of Korea, Norway and the United States.
ISTC facilitates international science projects and assists the global scientific and business community to source and engage with CIS and Georgian institutes that develop or possess an excellence of scientific know-how.