Ablation Model Based on Porous Charring Layer Under Alumina Erosion Condition
Ablation Predictions for Carbonaceous Materials Using Two Databases for Species Thermodynamics
Absolute rate constant measurements for the radiative combination ofatomic oxygen with nitric oxide
Acoustic Response of Near-Equilibrium Diffusion Flames with Large Activation Energies
The interaction of non-premixed flamelets with acoustic pressure waves of large characteristic wavelength, central to the development of
...Acoustic Suppression in a Pulsed Chemical Laser
Active Subspace Variation and Modeling Uncertainty in a Supersonic Flame Simulation
Advances in Computational Fluid Dynamics Methods for Hypersonic Flows
Over the past two decades or so, there have been many advances in the numerical simulation of hypersonic flows, with most effort focused
...Aerocapture Assessment for NASA Ice Giants Pre-Decadal Survey Mission Study
Aerodynamic Analysis of an Entry Capsule at Titan in Transition Regime
Aerodynamic Design of Nozzles with Uniform Outflow for Hypervelocity Ground-Test Facilities
A method is proposed for the aerodynamic design of nozzles with uniform outflow for supersonic and hypersonic ground-test facilities
...Aerothermodynamic Analysis of High-Altitude Space Launcher with Direct-Simulation Monte Carlo Method
Aerothermodynamics Behind a Blunt Body at Superorbital Speeds
Afterburning Effects on Thermal Environment of Liquid Oxygen/Kerosene Rocket Under Low Altitudes
Aluminum Oxide–Supported Manganese Oxide Catalyst for a 98% Hydrogen Peroxide Thruster
A model of chemical releases leading to upper-atmospheric chemi-ion formation.
Analogy Between Vibrational and Chemical Nonequilibrium Effects on Stagnation Flows
The vibrational excitation and chemical reaction of diatomic molecules are two typical real gas effects that can significantly influence
...Analysis of a High-Efficiency Low-Emissions "Chemical Gas Turbine" System
Analysis of Energy Utilization for Chemical Rockets
Methodology is developed for the comprehensive analysis and quantification of energy utilization in chemical rockets, based on the
...Analysis of Plume Infrared Signatures of S-Shaped Nozzle Configurations of Aerial Vehicle