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LARC Wind Tunnel Test Capabilities Facilities 20230517 - AIAA Niagara Frontier Presentation
X-59 Sonic Boom Test Results from the NASA Glenn 8- by 6-Foot Supersonic Wind Tunnel
X-59 Sonic Boom Test Results from the NASA Glenn 8- by 6-Foot Supersonic Wind Tunnel
Open Rotor Research at NASA Glenn
Free-flight and free-oscillation techniques for wind-tunnel dynamic-stability testing
NASA Environmentally Responsible Aviation Hybrid Wing Body Flow-Through Nacelle Wind Tunnel CFD
Overview of the Integrated Adaptive Wing Technology Maturation Wind-Tunnel Test Objectives
Comparison of the CHARM Predictions of the Multirotor Test Bed with Wind Tunnel Experimental Results
SLD Instrumentation in IWTs – Investigation Overview
Wind Tunnels. January, 1976-January, 1981 (Citations from the Energy Data Base)
Experimental Characterization of an Electric Ducted Fan for the SUSAN 25% Scale Research Vehicle
Extending the 15in x 15in Arizona Supersonic Wind Tunnel to Transonic Conditions
Tiltwing Validation Test: Conceptual Design and Research Objectives
Advancing Test Capabilities at NASA Wind Tunnels