Ablation Model Based on Porous Charring Layer Under Alumina Erosion Condition
Ablation Predictions for Carbonaceous Materials Using Two Databases for Species Thermodynamics
About the interaction between composition and performance of alternative jet fuels
About the interaction between composition and performance of alternative jet fuels
Absolute rate constant measurements for the radiative combination ofatomic oxygen with nitric oxide
Accounting for laminar run and trip drag in supersonic cruise performance testing
A chemically informed, control-oriented model of a three-way catalytic converter
A chemically informed, control-oriented model of a three-way catalytic converter
A Chemosorption Vacuum Pump for a Chemical Oxygen Iodine Laser with CO2 Buffer Gases
A comparison of tailpipe, dilution tunnel, and wind tunnel data in measuring motor vehicle PM
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
A decontamination system for chemical weapons agents using a liquid solution on a solid sorbent
A diesel particulate filter regeneration model with a multi-step chemical reaction scheme
A direct injection diesel combustion model for use in transient condition analysis
Adjustment of Regional Regression Equations for Urban Storm-Runoff Quality Using At-Site Data
Advanced treatment of recalcitrant textile wastewater and goal-oriented process design
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
...Aero Engine Ceramics—the Vision, the Reality and the Progress
Aerothermodynamic Analysis of High-Altitude Space Launcher with Direct-Simulation Monte Carlo Method
Aerothermodynamic Assessment of Spiked Configuration for Drag Reduction at Hypersonic Speeds
Aerothermodynamics Behind a Blunt Body at Superorbital Speeds
A field test study of leaf contamination on railhead surfaces
A finite-volume-based two-dimensional wall-flow diesel particulate filter regeneration model
Afterburning Effects on Thermal Environment of Liquid Oxygen/Kerosene Rocket Under Low Altitudes
A fundamental tribochemical study of the third body layer formed during automotive friction braking
A gas handling system for MOMBE growth
Aggregate Polishing Resistance Pre-Evaluation
Aging characterization of metals for exhaust systems
Aging characterization of metals for exhaust systems
Aircraft crash fire fighting by helicopter