Thermal Protection Materials: Development, Characterization and Evaluation
LEAPTech/HEIST Experiment Test and Evaluations Lessons Learned [STUB]
Structural Implementations of Leading-Edge Noise Reduction Devices
Lift Production on Flapping and Rotary Wings at Low Reynolds Numbers
Noise Reduction Through Circulation Control
Overview of Low-Speed Aerodynamic Tests on a 5.75% Scale Blended-Wing-Body Twin Jet Configuration
Calculation of the Flow About Wings of Arbitrary Planform at a Wide Range of Angles of Attack
Effect of Wing Tip Shape on Vortex Sheet Rolling Up
Transition Flight Experiments on a Swept Wing With Suction
Flutter Suppression and Gust Alleviation Using Active Controls
Lift Optimization Study of a Multi-Element Three-Segment Variable Camber Airfoil
Data Analytics to Support Operational Decision (Study Abstract)
A Feasibility Study of Heat-Pipe-Cooled Leading Edges for Hypersonic Cruise Aircraft