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
Extending the Leading-Edge Suction Analogy to Nonslender Delta Wings
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
Scaling Laws for Three-Dimensional Combined Heaving and Pitching Propulsors
Effect of Yaw Angle on Flutter of Rectangular Plates at Low Supersonic Speeds
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
Tip Clearance Effects on Cavitation Evolution and Head Breakdown in Turbopump Inducer
Simulation Methodologies of Engine Noise Shielding by Wings Within Conceptual Aircraft Design
Droplet Ratio Deformation Model in Combination with Droplet Breakup Onset Modeling
Effects of Small Leading-Edge Bluntness on High-Speed Boundary-Layer Instabilities on Flat Plates
Circulation Redistribution in Leading-Edge Vortices with Spanwise Flow
Optimized Permeability of Microporous Foam for Transpiration Cooling in Hypersonic Leading Edge
Visualization of Simulated Fuel–Air Mixing in a Dual-Mode Scramjet
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
Laser-Induced Plasma Ignition in a Cavity-Based Scramjet Combustor
Low-Noise Blade Design Optimization for a Transonic Fan Using Adjoint-Based Approach
Tones Encountered with a Coannular Nozzle and a Method for Their Suppression
HIFiRE-5b Boundary-Layer Transition Length and Turbulent Overshoot
Modeling of Droplet Deformation Near the Leading Edge of an Airfoil
Heat Transfer Measurements in Leading-Edge Cooling Geometry Under Rotating Conditions
Secondary Side Considerations for Boundary Layer Transition Flight Experiment
Boundary Layer Transition Preflight Experiments in a Mach-6 Quiet Tunnel
A Coupled Inviscid–Viscous Airfoil Analysis Solver, Revisited
Control of Dynamic Stall over a NACA 0015 Airfoil Using Plasma Actuators
Experimental Investigation of the Sound Emission of Skewed Axial Fans with Leading-Edge Serrations
Transverse Injection Through Diamond and Circular Ports into a Mach 5.0 Freestream
Laminar–Turbulent Transition Reversal on a Blunted Plate with Various Leading-Edge Shapes
Flow Separation Control over a Thin Post-Stall Airfoil: Effects of Excitation Frequency
Experimental Investigation of Supercooled Water Droplet Breakup near Leading Edge of Airfoil
Experimental Characterization of Three-Dimensional Scramjet Inlet with Variable Internal Contraction
Marine propeller blade tip flows