3D Representation of UAV-obstacle Collision Risk Under Off-nominal Conditions
3D Representation of UAV-obstacle Collision Risk under off-nominal conditions
4D BADA-based Trajectory Generator and 3D Guidance Algorithm
4. Parallels in Communication and Navigation Technology and Natural Phenomenon
8- by 6-Foot Supersonic Wind Tunnel Compressor Inspected
9- by 15-Foot Low Speed Wind Tunnel Acoustic Improvements Expanded Overview
9-Ft By 7-Ft Supersonic Wind Tunnel Nozzle Improvement Study
70 Years of Aeropropulsion Research at NASA Glenn Research Center
1991 International Conference on Aging Aircraft and Structural Airworthiness