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
X-43A Flight-Test-Determined Aerodynamic Force and Moment Characteristics at Mach 7.0
Workshop report for the AIAA 6th Aeroacoustics Conference
Workshop report for the AIAA 5th 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
...Wind-Tunnel Sonic-Boom Testing Techniques
When Are Allowables Conservative?
Aircraft designers are legally required to treat manufacturing variability so as to minimize the probability of structural failure
...What Was Learned in Predicting Slender Airframe Aerodynamics with the F-16XL Aircraft
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
...Wavelet Analysis of a Blade Tip-Leakage Flow
Waveform Transition of Sonic Boom Generated from a Sphere at Hypersonic Speed
Water-augmented turbofan engine
Wall Pressure Fluctuations Beneath Hypersonic Boundary Layer over Plate
Wall pressure fluctuations beneath a boundary layer are the main cause of structural vibration for hypersonic aircraft. To accurately
...Wall-Mounted Finite Airfoil-Noise Production and Prediction
This paper presents the results of an experimental investigation of the flow-induced sound produced by a smooth, wall-mounted finite
...Wall-Modeled Large-Eddy Simulation with Second-Order-Accurate Upwind Scheme
In aircraft aerodynamic design, it is essential for certification by analysis to estimate aircraft aerodynamic characteristics with high
...Wall-Modeled Large-Eddy Simulation of Transonic Buffet over NASA-CRM Using FFVHC-ACE
This study investigates the capability of wall-modeled large-eddy simulation (WMLES) in predicting the transonic buffet phenomenon over
...Wall curvature and transition effects in turbulent boundary layers
Wake Vortex Encounter Risk Assessment for Crosswind Departures
Wake Sensing and Estimation for Control of Autonomous Aircraft in Formation Flight
Wake Impact Alleviation Control Based on Wake Identification
Vortical singularities in conical flow.
Vortex Shedding from Airfoils in Reverse Flow
Vortex interactions and decay in aircraft wakes
Vortex interactions and decay in aircraft wakes
Vortex Identification and Quantification on Blunt Trailing-Edge Rotor Blades in Reverse Flow
An inherent aerodynamic limitation of high-advance-ratio high-speed helicopters is reverse flow on the retreating blades, which can be a
...Vortex Buffeting of Aircraft Tail: Interpretation via Proper Orthogonal Decomposition
Vortex breakdown - Tail interaction
Volumetric Velocimetry of Complex Geometry Effects on Transonic Flow over Cavities
Vibroacoustic Modes and Active Control of Both Vibration and Sound
Vibration Analysis of Curvilinearly Stiffened Composite Panel Subjected to In-Plane Loads
This paper presents an efficient finite element approach to study the prestressed vibration mode results of a curvilinearly stiffened
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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
...Verification of the Transition Model in OVERFLOW and FUN3D
The findings of the recent AIAA and NATO workshops on transition modeling have underscored the importance of verifying the transition
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