Unsteady effect of shock wave induced separation.

Aerodymanic Validation of Emission Reducing Technologies.

The new generation of CS-23 category aircraft - Cost Effective Small AiRcraft.

Interoperable Management of Aeronautical Generic Executive Software

Joint Cypriot-Romanian Air Pollution Dispersion Research Studies for EU Harmonization.

Placing satellite objects at low and medium altitudes still requires the consumption of very large financial and technical resources, which limits access to the utilities offered by such orbital stations (usually without human personnel).

The proposed project has as its major orientation the irrigation of agricultural surfaces located both in hilly areas and in plain areas, areas where the frequency and intensity of air currents is reduced. Unlike the high-power installations used in regions with high wind potential (mountainous and coastal areas), the project aims to capitalize on the lower wind potential, specific to the plain areas, which are the main agro-food sources.

The project is integrated into the current research, on an international level, regarding the creation of new, advanced materials with applications in top fields of the aerospace industry.

Aeronautical morphing structures are defined in specialized literature as intelligent structures with the ability to change their characteristics under the action of external stimuli.

New performance horizons of materials that operate in extreme conditions are accessible by accumulating and correlating the material expertise associations, now dispersed, in different applications in the aeronautical, space, steel, energy industries.

The micro-vehicles with flapping wings (MAB) are small aerial devices, designed for researching closed spaces, such as: buildings, tunnels, chimneys, etc. MAB can also take over other missions, this time outside, namely the execution of reconnaissance in dangerous areas, such as a contaminated land. The advantage of MAB lies in the fact that fixed-wing micro-air vehicles are too fast to maneuver between buildings.

Inorganic polymer-layered nanocomposites as reinforced hybrids at the nanometric scale.

The project aims to organize, develop and operate a specific infrastructure for regional air transport at the level of Romania and in the immediate vicinity, with major implications for regional development.

Structural health monitoring in spacecraft structures using piezoelectric wafer active sensors and multimodal guided waves.

Dynamic Launching and Recovery procedures from High Altitudes.

Hyperspectral Image Feature Extraction Tools.

INCAS Launcher and Space Vehicles Center of Competence – INCAS LASVEC.

Suborbital Launcher for Testing, Unconventional Subsystems Development.

Integrated Evaluation System for Advanced MulTilayered MateriaLs in AeroSpace and Related Fields.

Clouds and Aerosols Profiling in suport of ESA’s sentinel 4 and 5 missions

Inverse aero-thermodynamic  analysis for supersonic/hypersonic flows

Antiflutter Demonstrator with Piezoelectric Actuation/ Antiflutter Demonstrator with Piezoelectric Actuation

Computational Model for Prediction of "Biomass Burning" Emissions.

Advanced research to increase competitiveness and capacity for design, analysis and expertise specifically in the aerospace field.

In the context of fighting the COVID-19 pandemic, the tendency to use autonomous UAS-type systems is the right choice, since they allow the intervention of remote human operators in risk areas, without endangering the ground operational teams.

Lightweight reinforced thermoPLASTic MATerials for vacuum thermoformed encapsulation applications in Unmanned Aerial Vehicles.

Commercial aircraft and aviation in general face in flight the appearance of turbulent fields, which requires changes in airplane trajectory in order to avoid as much as possible the danger to aircraft and passengers.

The project aims to develop some contributions to the theory of delayed differential equations (DDE) and switched systems by developing, mainly, necessary and sufficient conditions for stability of equilibrium points and reducing the conservativeness of sufficient conditions given by the use of multiple Lyapunov-Krasovskii functionals.

INCAS has initiated an original methodology possible to be implemented in blowdown wind tunnels (e.g. INCAS Supersonic Wind Tunnel) and possible to be adapted for large industrial wind tunnels (e.g. NASA, TsAGI). However, additional research is needed to establish a credible scientific foundation for designing supersonic aircraft with low sonic booms and to develop improved experimental evaluation tools in relevant environment at higher TRL (TRL > 6).

The main objective of the project is designing, achieving and testing the prototype of an innovative UAS (Unmanned Aircraft System) TRL 8 level (complete system, certified by tests and demonstrations that will be used by the project beneficiary in specific national security enforcement applications).

In the last years, the worldwide impact of global change lead to the development of new and more precise Earth observation programme, able to provide accurate and timely information for improving the management of the environment.