European Experimental Reentry Testbed Winglet: From In-Flight Characterization to SCIROCCO Test
Evaluating Enhanced Boiling Heat Transfer in a Novel Grooved Tube
Evaluation of Next Generation Military Vehicle Cooling Systems
Evaluation of Wavy-Trailing-Edge Film Cooling Versus Pressure Side Cutback Cooling
Exergy Balance Decomposition Between Mechanically- and Thermally-Recoverable Exergy Outflows
Experimental and Numerical Study of Cooling Gas Injection in Laminar Supersonic Flow
Experimental Estimation of Energy Losses in Tapered Roller Bearings
Experimental Investigation of Mist Sprays Impinging on a Heated Cylinder
Experimental Study of Graphite Ablation in Nitrogen Flow, Part II: Further Numerical Analysis
Experimental Study on Pressure Drop of Aluminum-Oxide/Water Nanofluids
Feasibility Study of Aerocapture at Mars with an Innovative Deployable Heat Shield
Film Cooling Overall Effectiveness of Shaped Holes at Elevated Temperatures
Flight Set 360L001 (STS-26) Igniter, Post Flight
Flow Control of Swept Shock-Wave/Boundary-Layer Interaction Using Plasma Actuators
Flow-Tube Oxidation Experiments on the Carbon Preform of a Phenolic-Impregnated Carbon Ablator
Fluidic Control Method for Improving the Self-Starting Ability of Hypersonic Inlets
Gas-Phase Recombination Effect on Surface Heating in Nonequilibrium Hypersonic Flows
Graphite Ablation and Radiation on Interaction with Hypervelocity Earth-Entry Flows