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