Correction: Modeling of Droplet Deformation Near the Leading Edge of an Airfoil
The Second International Vortex Flow Experiment (VFE-2): Objectives and first results
Ultra-high temperature ceramics developments for hypersonic applications
LEAPTech/HEIST Experiment Test and Evaluations Lessons Learned [STUB]
Extending the Leading-Edge Suction Analogy to Nonslender Delta Wings
Structural Implementations of Leading-Edge Noise Reduction Devices
Thermal Protection Materials: Development, Characterization and Evaluation
Lift Production on Flapping and Rotary Wings at Low Reynolds Numbers
Supersonic Flutter Analysis Based on a Local Piston Theory
Inviscid Nonlinear Modeling of Vibration-Induced Acoustic Resonance of a Linear Cascade
Locating the Isolator Shock-Train Leading Edge with Limited Pressure Information
Investigation of a Porous Transpiration-Cooled Strut Injector
Waverider Design Based on Three-Dimensional Leading Edge Shapes
Effect of Yaw Angle on Flutter of Rectangular Plates at Low Supersonic Speeds
Scaling Laws for Three-Dimensional Combined Heaving and Pitching Propulsors
Heat Transfer and Secondary Flow with a Multicavity Gas Turbine Blade Tip
Modeling the Flow State Sensitivity of Actuation Response on a Stalled Airfoil
Effect of Vibrational Nonequilibrium on Isolator Shock Structure
Numerical Simulation of Transpiration Cooling for a High-Speed Vehicle with Substructure
Simulation Methodologies of Engine Noise Shielding by Wings Within Conceptual Aircraft Design
Effects of Small Leading-Edge Bluntness on High-Speed Boundary-Layer Instabilities on Flat Plates
Circulation Redistribution in Leading-Edge Vortices with Spanwise Flow
Visualization of Simulated Fuel–Air Mixing in a Dual-Mode Scramjet
Optimized Permeability of Microporous Foam for Transpiration Cooling in Hypersonic Leading Edge
Noise Reduction Through Circulation Control
Wall Distance Effects on Transition to Turbulence in Low-Reynolds-Number Separated Flows
Characterization of Cavitation Instabilities in a Four-Bladed Turbopump Inducer
Response of Shock Train to High-Frequency Fluctuating Backpressure in an Isolator
Effect of Wing Tip Shape on Vortex Sheet Rolling Up
Tip Clearance Effects on Cavitation Evolution and Head Breakdown in Turbopump Inducer
Low-Noise Blade Design Optimization for a Transonic Fan Using Adjoint-Based Approach
Transition Flight Experiments on a Swept Wing With Suction
Droplet Ratio Deformation Model in Combination with Droplet Breakup Onset Modeling
Secondary Side Considerations for Boundary Layer Transition Flight Experiment
Heat Transfer Measurements in Leading-Edge Cooling Geometry Under Rotating Conditions
Calculation of the Flow About Wings of Arbitrary Planform at a Wide Range of Angles of Attack
Boundary Layer Transition Preflight Experiments in a Mach-6 Quiet Tunnel
A Coupled Inviscid–Viscous Airfoil Analysis Solver, Revisited
Experimental Investigation of the Sound Emission of Skewed Axial Fans with Leading-Edge Serrations
Control of Dynamic Stall over a NACA 0015 Airfoil Using Plasma Actuators