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]
Structural Implementations of Leading-Edge Noise Reduction Devices
Extending the Leading-Edge Suction Analogy to Nonslender Delta Wings
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
Investigation of a Porous Transpiration-Cooled Strut Injector
Locating the Isolator Shock-Train Leading Edge with Limited Pressure Information
Scaling Laws for Three-Dimensional Combined Heaving and Pitching Propulsors
Heat Transfer and Secondary Flow with a Multicavity Gas Turbine Blade Tip
Effect of Yaw Angle on Flutter of Rectangular Plates at Low Supersonic Speeds
Modeling the Flow State Sensitivity of Actuation Response on a Stalled Airfoil
Waverider Design Based on Three-Dimensional Leading Edge Shapes
Effects of Small Leading-Edge Bluntness on High-Speed Boundary-Layer Instabilities on Flat Plates
Low-Noise Blade Design Optimization for a Transonic Fan Using Adjoint-Based Approach
Effect of Vibrational Nonequilibrium on Isolator Shock Structure
Noise Reduction Through Circulation Control
Optimized Permeability of Microporous Foam for Transpiration Cooling in Hypersonic Leading Edge
Calculation of the Flow About Wings of Arbitrary Planform at a Wide Range of Angles of Attack
Circulation Redistribution in Leading-Edge Vortices with Spanwise Flow
Numerical Simulation of Transpiration Cooling for a High-Speed Vehicle with Substructure
Secondary Side Considerations for Boundary Layer Transition Flight Experiment
A Coupled Inviscid–Viscous Airfoil Analysis Solver, Revisited
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
Simulation Methodologies of Engine Noise Shielding by Wings Within Conceptual Aircraft Design
Control of Dynamic Stall over a NACA 0015 Airfoil Using Plasma Actuators
Transition Flight Experiments on a Swept Wing With Suction
Droplet Ratio Deformation Model in Combination with Droplet Breakup Onset Modeling
Heat Transfer Measurements in Leading-Edge Cooling Geometry Under Rotating Conditions
Visualization of Simulated Fuel–Air Mixing in a Dual-Mode Scramjet
Experimental Investigation of Supercooled Water Droplet Breakup near Leading Edge of Airfoil
Laser-Induced Plasma Ignition in a Cavity-Based Scramjet Combustor