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