Experimental and Numerical Study of Cooling Gas Injection in Laminar Supersonic Flow
Surface Heating and Boundary-Layer Transition on a Hypersonic Inflatable Aerodynamic Decelerator
Coupled Zero-Dimensional/One-Dimensional Model for Hybrid Heat Transfer Measurements
Computational Modeling of a Segmented-Involute-Foil Regenerator for Stirling Engines
Acoustic Response of a Resonant Igniter with Confuser Inlet
Start-Up Analysis of a Hypersonic Short-Duration Facility
Investigation of Freestream Plasma Flow Produced by Inductively Coupled Plasma Wind Tunnel
Acoustic Interferometry and the Calibration Integral Equation Method for Inverse Heat Conduction
Edge-Based Finite Element Formulation of Hypersonic Flows Under an Imposed Magnetic Field
Validation of a Zonal Approach Computing the Sound Radiation from Lined Ducts
Aerodynamic Analysis of Total Temperature Probe Thermal Performance Using Conjugate Heat Transfer
Assessing Hypersonic Boundary-Layer Stability in the Presence of Structural Deformation
Model of Film Condensation on a Vertical Plate with Noncondensing Gas
Heat Flux Duplication Between Ground Facility and Hypersonic Flight
Hexcomb-Pattern Roughness Effects on Blunt-Body Transition and Heating
Simulation of Second-Mode Instability in a Real-Gas Hypersonic Flow with Graphite Ablation
Stabilization of a Mach 5.92 Boundary Layer by Two-Dimensional Finite-Height Roughness