Add to ORKGIncluded are slides used in the design review for the mAEWing1 vehicle as part of the Performance Adaptive Aeroelastic Wing program, held February 27, 2015.NASA NRA, "Lightweight Adaptive Aeroelastic Wing for Enhanced Performance Across the Flight Envelope," NRA NNX14AL36A, Mr. Daniel Moerder Technical Monitor
This working paper documents an initial control feasibility study to determine if classical control ...
Testing and evaluation of a stability augmentation system for aircraft flight control were performed...
This is Part 2-Appendices of a study conducted under Drones for Aerodynamic and Structural Testing (...
Included are slides used in the kickoff meeting for the Performance Adaptive Aeroelastic Wing progra...
Included is the presentation for the NASA High Aspect Ratio Wing (HARW) NRA Year 1 Review. Programma...
This presentation to be presented at Boeing Technical Interchange Meeting in Mukilteo, WA gives an o...
An overview of recent aeroelasitc wing-shaping work at the NASA Ames Research Center is presented. T...
Successful flight-testing of the Active Aeroelastic Wing airplane was completed in March 2005. This ...
Research pilots have flown the Mission Adaptive Wing (MAW) aircraft, a highly modified F-111 jet fig...
The Active Aeroelastic Wing research program was a joint program between the U.S. Air Force Research...
NASA has had a long history in fundamental and applied high lift research. Current programs provide ...
The wing on the NASA F-111 transonic aircraft technology airplane was modified to provide flexible l...
Armstrong (formerly Dryden) Flight Research Center continues it's legacy of exciting work in the are...
Recent research on advanced-configuration commercial aircraft at DFVLR is surveyed, with a focus on ...
Aerodynamic and active control concepts for application to commercial transport aircraft are discuss...
This working paper documents an initial control feasibility study to determine if classical control ...
Testing and evaluation of a stability augmentation system for aircraft flight control were performed...
This is Part 2-Appendices of a study conducted under Drones for Aerodynamic and Structural Testing (...
Included are slides used in the kickoff meeting for the Performance Adaptive Aeroelastic Wing progra...
Included is the presentation for the NASA High Aspect Ratio Wing (HARW) NRA Year 1 Review. Programma...
This presentation to be presented at Boeing Technical Interchange Meeting in Mukilteo, WA gives an o...
An overview of recent aeroelasitc wing-shaping work at the NASA Ames Research Center is presented. T...
Successful flight-testing of the Active Aeroelastic Wing airplane was completed in March 2005. This ...
Research pilots have flown the Mission Adaptive Wing (MAW) aircraft, a highly modified F-111 jet fig...
The Active Aeroelastic Wing research program was a joint program between the U.S. Air Force Research...
NASA has had a long history in fundamental and applied high lift research. Current programs provide ...
The wing on the NASA F-111 transonic aircraft technology airplane was modified to provide flexible l...
Armstrong (formerly Dryden) Flight Research Center continues it's legacy of exciting work in the are...
Recent research on advanced-configuration commercial aircraft at DFVLR is surveyed, with a focus on ...
Aerodynamic and active control concepts for application to commercial transport aircraft are discuss...
This working paper documents an initial control feasibility study to determine if classical control ...
Testing and evaluation of a stability augmentation system for aircraft flight control were performed...
This is Part 2-Appendices of a study conducted under Drones for Aerodynamic and Structural Testing (...