Compact analogs of the models of vortex flows generated by aircraft flight
Numerical Investigation of Droplet Properties of a Liquid Jet in Supersonic Crossflow
Design and implementation of hardware-in-the-loop (HIL) test-bed for spacecraft attitude control
Tabletop Testbed for Attitude Determination and Control of Nanosatellites
TO THE STUDY OF WAKE VORTEX BEHIND THE AIRBUS-380 CHARACTERISTICS AT TAKEOFF AND LANDING
Parametric investigation of acoustic radiation by a beam under load and actuator forces
Investigation of acoustic field near to elastic thin plate using integral method