Structural Implementations of Leading-Edge Noise Reduction Devices
Heat Transfer and Secondary Flow with a Multicavity Gas Turbine Blade Tip
Calculation of the Flow About Wings of Arbitrary Planform at a Wide Range of Angles of Attack
Optimized Permeability of Microporous Foam for Transpiration Cooling in Hypersonic Leading Edge
Transition Flight Experiments on a Swept Wing With Suction
Heat Transfer Measurements in Leading-Edge Cooling Geometry Under Rotating Conditions
Direct Simulation Monte Carlo Modeling of Gas Electronic Excitation for Hypersonic Sensing
Non-Newtonian Fluid Flow on a Flat Plate Part 1: Boundary Layer
Thermal Considerations with Respect to Sliding Contact at High Speed
Thermostructural Responses of Metallic Lattice-Frame Sandwich Structure for Hypersonic Leading Edges
Assessment of Limiting Processes of Numerical Schemes on Hypersonic Aeroheating Predictions
Entropy Generation in Nonisothermal Flows: Influence of Boundary Condition Type and Intensity
Electrohydrodynamic-Enhanced Natural Convection in an Enclosure by a Nonsymmetric Electric Field
Numerical Study of Swirl Cooling in a Turbine Blade Leading-Edge Model
Turbine Blade Tip and Casing Phantom Cooling from Blade-Surface Film Coolant
Non-Newtonian Fluid Flow on a Flat Plate Part 2: Heat Transfer