In the upcoming decade, ground-to-space laser links will become abundant in scientific and industrial applications and Unmanned Aerial Vehicles (UAV)
Aerofoil self-noise produced by flow separation and stall is relatively little understood regarding the underlying generation mechanisms. The focus of
While SHM science and engineering have matured in recent decades, by now indeed a coherent and well-established branch of structural
A guided rocket system performance is often evaluated by solving an optimal control problem which minimizes a pre-defined objective function,
Flight control law clearance provides the conditions needed for the system to operate in the stability boundaries. One way to
Simulation of dynamic response of Aero-Servo-Elastic Wind-Tunnel model to Non-Uniform gust was conducted. The research is done under the “Gust
Numerous animals including fish, birds, bats and insects use appendages (fins and wings) with varying levels of flexibility, to provide
The simulation of the aerothermal environment surrounding vehicles moving at hypersonic speed is a complex problem due to its multi-physics
Micro gas turbines generally employ uncooled turbine blades and their thrust is limited by the maximum allowable gas temperature. A
During the design phase of a project, each airborne system is designed and tested in order to demonstrate it can
The commercial aviation industry is motivated to continuously improve landing performance without involving radical changes to aircraft design or operation.
High-enthalpy arc-heated supersonic wind tunnels are characterized by test gases that are heated by a high-current electric arc and then
Multirotor UAVs are becoming widespread for both civil and military uses, such as photography, surveillance and payload transportation. A slung
The main goals in aircraft design nowadays are noise and emission reduction, together with performance improvement. These can be achieved
This talk outlines an effort to understand the impact of inlet isolator physics on the combustion of scramjet engines under
In a general research setting, theoretical models combined with simulation provide the backbone for guidance, navigation, and control systems design.
Fuel supply in microjet engines typically makes use of fuel vaporizers. These have a simple design however, their operation involves
In recent years, the use of multi-rotors has been drastically increased both in military and civil applications. Specifically, load transportation
Classification and object recognition is a fundamental problem in many robotics and aerospace applications, such as autonomous driving, vision-based navigation,
Capacitively coupled radio-frequency thrusters (CCRFT) are an attractive propulsion option for nanosatellites due to their low operating power, relatively high
Ignition is a challenge for gas turbines, ramjets and scramjets where flow velocities in the combustor are high, resulting in
Destructive vibrations caused by stochastic external disturbances such as earthquakes, explosions, and fluid-structure interactions pose an insidious threat to various
The supersonic combustion ramjet, or scramjet, is an air-breathing engine designed for cruise at Mach number of 5 and above.
Investigation of the performance of experimental combustion devices relies heavily on proper diagnostics for characterization of operating regimes and validation
A crucial part of the development of a complex system is its testing and validation. To support the design and
A major current threat on Unmanned Aerial Vehicles (UAVs) and Air-to-Surface Missiles (ASM) is being intercepted by Surface-to-Air Missiles (SAMs)
Grid fins are actually an array of short lifting surfaces arranged in a lattice. They appeared in engineering literature in
Through natural selection, animals evolved the abilities required to survive in a complex dynamic world: they accurately perceive their surroundings,
