Zonal Detached Eddy Simulations of a Dual-Stream Jet: Turbulence Rate Sensitivity
Zonal Detached Eddy Simulations of a Dual-Stream Jet: Turbulence Rate Sensitivity
Zonal Detached Eddy Simulations of a Dual-Stream Jet: Turbulence Rate Sensitivity
Zonal Detached-Eddy Simulations of a Dual-Stream Jet
Zonal Detached-Eddy Simulations of a Dual-Stream Jet
Zonal Detached-Eddy Simulation of Separated Flow Around a Finite-Span Wing
Zonal Detached Eddy Simulation of a Civil Aircraft with a Deflected Spoiler
Zonal Detached Eddy Simulation of a Civil Aircraft with a Deflected Spoiler
YOLOv4 Object Detection Model for Nondestructive Radiographic Testing in Aviation Maintenance Tasks
X-HALE: A Very Flexible Unmanned Aerial Vehicle for Nonlinear Aeroelastic Tests
Workshop report for the AIAA 6th Aeroacoustics Conference
Workshop report for the AIAA 5th Aeroacoustics Conference
Workshop Report for the 4th AIAA Aeroacoustics Conference
Within Homogeneous Turbulence: Crow Instability Large Eddy Simulation of Aircraft Wake Vortices
Wing-tip vortices, turbulence, and the distribution of emissions
Wing Tip Vortices from an Exergy-Based Perspective
Wind-Tunnel Testing of Otto Lilienthal’s Production Aircraft from 1893
A full-scale wind-tunnel test of a replica of Otto Lilienthal’s Normalsegelapparat from 1893 was conducted in a closed
...Wind Tunnel System for Active Flutter Suppression Research: Overview and Insights
This paper describes the development of a new state-of-the-art large wind tunnel model for active flutter suppression studies as well as
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When Are Allowables Conservative?
Aircraft designers are legally required to treat manufacturing variability so as to minimize the probability of structural failure
...Weight Indexing for Wing-Shape Multi-Objective Optimization
Weight Indexing for Wing-Shape Multi-Objective Optimization
Weighted Gradient-Enhanced Kriging for High-Dimensional Surrogate Modeling and Design Optimization
A novel formulation of gradient-enhanced surrogate model, called weighted gradient-enhanced kriging, is proposed and used in combination
...Waverider Design Using Osculating Method
Because of the requirements of payload capability, flight range, and maneuverability, hypersonic aircraft demand high aerodynamic
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