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title: AIAA Journal of Aircraft
Aeroacoustic Performance of Fractal Spoilers
Aeroacoustic Prediction of a Multi-Element Airfoil Using Wall-Modeled Large-Eddy Simulation
Aeroacoustic Prediction of a Multi-Element Airfoil Using Wall-Modeled Large-Eddy Simulation
Aeroacoustic Simulations of a Simplified High-Lift Device Accounting for Some Installation Effects
The aeroacoustic noise of a simplified wing-flap configuration placed in an open-jet anechoic wind tunnel is investigated by
...Aerodynamic Analysis and Optimization of Embedded Slot for Smooth Morphing Trailing Edge
Aerodynamic Analysis of a Flapping Rotary Wing at a Low Reynolds Number
Aerodynamic Comparison of Freezing Rain and Freezing Drizzle Conditions at the RTA Icing Wind Tunnel
Aerodynamic Data Fusion Toward the Digital Twin Paradigm
Aerodynamic Effects of Propeller Slipstream on a Wing with Circulation Control
Aerodynamic interactions between adjacent slender bodies
Aerodynamic optimization of a morphing airfoil using energy as an objective
Aerodynamic Optimization of Essentially Three-Dimensional Shapes for Wing-Body Fairing
Aerodynamic Optimization over Frigate Helicopter Flight Deck by Hangar Shape Modifications
Helicopter operations on frigates imply complex maneuvers for pilots. During the aircraft approach to the frigate, the helicopter rotor
...Aerodynamic Parameter Identification and Uncertainty Quantification for Small Unmanned Aircraft
Aerodynamic Prediction of High-Lift Configuration Using Turbulence Model
The aerodynamic performance of the high-lift configuration greatly influences the safety and economy of commercial aircraft. Accurately
...Aerodynamic Prediction of Iced Airfoils Based on Modified Three-Equation Turbulence Model
Ice formation on a wing poses a threat to aircraft safety because it changes the effective shape of the wing and considerably
...Aerodynamic Prediction of the High-Lift Common Research Model with Modified Turbulence Model
Aerodynamic Shape Optimization Investigations of the Common Research Model Wing Benchmark
Aerodynamic Shape Optimization of Aircraft Wings Using Panel Methods
Aerodynamic Shape Optimization of Natural-Laminar-Flow Wing Using Surrogate-Based Approach
Aerodynamic shape optimization of a swept natural-laminar-flow wing in the transonic regime is still challenging. The difficulty is
...Aeroelastic-acoustics simulation of flight systems