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2010-4360 Application of the Boundary Layer Data System on a Laminar Flow Swept Wing Model In Flight
STEP EXCRESCENCE EFFECTS FOR MANUFACTURING TOLERANCES ON LAMINAR FLOW WINGS
AN APPROACH TO MEASURING STEP EXCRESCENCE EFFECTS IN A PRESSURE GRADIENT
Transition due to Surface Steps in the Presence of Favorable Pressure Gradients
Development and Flight Demonstration of Self-Contained Boundary Layer Measurement Devices
Transition in Incompressible Boundary Layers with Two-Dimensional Excrescences
Design of a Third-Generation Boundary Layer Measurement System for In-Flight Measurements
A Compact, Self-Contained System for Boundary Layer Measurements in Flight
Contemporary issues affecting the demand for business air travel in the United States
Digitale Schutz- und Stationsleittechnik in Industrienetzen