Data Summary from the First AIAA Computational Fluid Dynamics Drag Prediction Workshop
Boundary Layer Ingestion Benefit of the D8 Transport Aircraft
Boundary Layer Ingestion Benefit of the D8 Transport Aircraft
NSU3D Results for the Second AIAA High-Lift Prediction Workshop
Constructal Design of Flying Wing Aircraft: Curved and Swept Configurations
Study of Droplet Shadow Zone of Aircraft Wing with Diffusion Effects
The aircraft deicing and detection tasks are complicated by the revealed existence of a shadow zone behind the wings, which contains no
...High-Fidelity Modeling of Multirotor Aerodynamic Interactions for Aircraft Design
Electric aircraft technology has enabled the use of multiple rotors in novel concepts for urban air mobility. However, multirotor
...AIAA Manuscript Review Process
Acoustics of Aircraft Engine-Duct Systems
Vertical Drop Test of Composite Fuselage Section of a Regional Aircraft
In this paper, a vertical drop test of a full composite fuselage section of a regional aircraft has been presented. This test was
...Geometric Programming for Aircraft Design Optimization
Formulating conceptual-stage aircraft design problems as geometric programs, which are a specific type of convex optimization problem
...Three-Way Spectral Decompositions of High-Performance Military Aircraft Noise
Source Localization of Crackle-Related Events in Military Aircraft Jet Noise
AIAA Manuscript Review Process
Global/Local Optimization of Aircraft Wing Using Parallel Processing
The structural optimization of a cantilever aircraft wing with stiffeners and curvilinear spars and ribs is described. The decomposition
...Global/Local Optimization of Aircraft Wing Using Parallel Processing
Global/Local Optimization of Aircraft Wing Using Parallel Processing
AIAA Manuscript Review Process
Aircraft Icing Severity Analysis Considering Three Uncertainty Types
Flight Performance with Respect to Rotor Rotation Directions of Multirotor Aircraft
AIAA Manuscript Review Process
Noise characteristics of aircraft high lift systems
AIAA Manuscript Review Process