Heat Transfer and Temperature Analysis of an Aeroengine Strut Under Icing Conditions
Characterization of a Large-Scale Arcjet Facility Using Tunable Diode Laser Absorption Spectroscopy
Thermal Analysis and Testing of Nonrotating Cone with Hot-Air Anti-Icing System
Stabilization of Premixed Swirl Flames Under Flow Pulsations Using Microsecond Pulsed Plasmas
Blunt-Body Paradox and Improved Application of Transient-Growth Framework
Characterization of Structural Response to Hypersonic Boundary-Layer Transition
Investigations of Base Thermal Environment on Four-Nozzle Liquid Launch Vehicle at High Altitude
Radiative Heating During Mars Science Laboratory Entry: Simulation, Ground Test, and Flight
Effects of Chemistry in Nonequilibrium Hypersonic Flow Around Blunt Bodies
Numerical Simulation of Stagnation Line Nonequilibrium Airflows for Reentry Applications
Influence of Single Roughness Element on Hypersonic Boundary-Layer Transition of Cone
Study of the Liquid Breakup Process in Solid Rocket Motor
Hybrid Particle-Continuum Simulations of Hypersonic Flow Over a Hollow-Cylinder-Flare Geometry
Hypersonic Boundary-Layer Instability Characteristics on Sharp Cone with Porous Coating
Modeling Heat-Shield Erosion due to Dust Particle Impacts for Martian Entries
Tool for Rapid Transient Transpiration-Cooled Reentry Simulation
Prediction of Nonequilibrium Air Plasma Radiation Behind a Shock Wave
Reverse Design of Ultrasonic Absorptive Coating for the Stabilization of Mack Modes
Experimental and Numerical Study of Cooling Gas Injection in Laminar Supersonic Flow
Assessment of Limiting Processes of Numerical Schemes on Hypersonic Aeroheating Predictions
Molecular-Dynamics-Derived Gas–Surface Models for Use in Direct-Simulation Monte Carlo
Coupled Zero-Dimensional/One-Dimensional Model for Hybrid Heat Transfer Measurements
Aeroelastic Analysis of Pinched Panels in Supersonic Flow Changing with Altitude
Surface Heating and Boundary-Layer Transition on a Hypersonic Inflatable Aerodynamic Decelerator
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
Model of Film Condensation on a Vertical Plate with Noncondensing Gas
Assessing Hypersonic Boundary-Layer Stability in the Presence of Structural Deformation
Heat Flux Duplication Between Ground Facility and Hypersonic Flight
Simulation of Second-Mode Instability in a Real-Gas Hypersonic Flow with Graphite Ablation
Hexcomb-Pattern Roughness Effects on Blunt-Body Transition and Heating
Stabilization of a Mach 5.92 Boundary Layer by Two-Dimensional Finite-Height Roughness
Knock criteria for aviation diesel engines
Modeling In-Flight Ice Accretion Under Uncertain Conditions
Efficient Two-Way Coupled Analysis of Steady-State Particle-Laden Hypersonic Flows
Assessment of the Reconstructed Aerodynamics of the Mars Science Laboratory Entry Vehicle
Uncertainty Analysis of Radiative Heating Predictions for Titan Entry
Local Solution to the Unsteady Stefan Problem for In-Flight Ice Accretion Modeling