Influence of density ratio between liquid and gas on sloshing model test results
Aerodynamic performance of an over-the-wing propeller configuration at increasing Mach number
Aerodynamic performance of an over-the-wing propeller configuration at increasing Mach number
Aerodynamic performance of an over-the-wing propeller configuration at increasing Mach number
Propulsion system integration and thrust vectoring aspects for scaled jet UAVs
Propulsion system integration and thrust vectoring aspects for scaled jet UAVs
Propulsion system integration and thrust vectoring aspects for scaled jet UAVs
In-Vehicle Network Security — MACsec, the game changer
Metamodeling for Effectiveness Based Aircraft Design Under Uncertainty (AIAA 2018-3743)