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