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