Alulema et al., 2020 - Google Patents
Performance assessment of a variable-span morphing wing small UAV for high altitude surveillance missionsAlulema et al., 2020
View PDF- Document ID
- 9059761629040785136
- Author
- Alulema V
- Valencia E
- Toapanta E
- Guailla C
- Pazmiño M
- Publication year
- Publication venue
- AIAA Propulsion and Energy 2020 Forum
External Links
Snippet
Morphing wings are of great interest to the unmanned aircraft community because they enable to modify the wing geometry during flight to adapt the performance of the UAV according to the flight conditions. Particularly, variable-span wings could enhance the …
- 238000011160 research 0 abstract description 15
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
- Y02T50/14—Adaptive structures
- Y02T50/145—Morphing wings or smart wings
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Ventura Diaz et al. | High-fidelity computational aerodynamics of multi-rotor unmanned aerial vehicles | |
EP3509944B1 (en) | Blade or wing | |
Kontogiannis et al. | Design, performance evaluation and optimization of a UAV | |
Selig | Modeling full-envelope aerodynamics of small UAVs in realtime | |
Vogeltanz | A survey of free software for the design, analysis, modelling, and simulation of an unmanned aerial vehicle | |
Jones et al. | Preliminary flight test correlations of the X-HALE aeroelastic experiment | |
Harmon | Aerodynamic modeling of a flapping membrane wing using motion tracking experiments | |
Colas et al. | HALE multidisciplinary design optimization part i: solar-powered single and multiple-boom aircraft | |
Chakraborty et al. | Sizing and Analysis of a Tilt-Wing Aircraft with All-Electric and Hybrid-Electric Propulsion Systems | |
Tarabi et al. | Experimental investigation of a variable-span morphing wing model for an unmanned aerial vehicle | |
Sivanandi et al. | A review on evolution of aeroelastic assisted wing | |
Della Vecchia et al. | Advanced turboprop multidisciplinary design and optimization within AGILE project | |
Jayakumar et al. | Design, control, aerodynamic performances, and structural integrity investigations of compact ducted drone with co-axial propeller for high altitude surveillance | |
Chakraborty et al. | Design and Sizing of a Dual-Purpose Hybrid-Electric Ducted Fan Lift-Plus-Cruise Aircraft | |
Salazar et al. | Defining a conceptual design for a tilt-rotor micro air vehicle for a well-defined mission | |
Alulema et al. | Performance assessment of a variable-span morphing wing small UAV for high altitude surveillance missions | |
Aksugur et al. | Design methodology of a hybrid propulsion driven electric powered miniature tailsitter unmanned aerial vehicle | |
Joels et al. | Design, Analyses, and Flutter Testing of the Active Aeroelastic Aircraft Testbed (A3TB) Platform | |
Saez et al. | Mars drone configurations and approaches to rotor design: a review | |
Langston et al. | Low-speed stability and control of a reduced scale long-range supersonic configuration with reduced-size or no vertical tail | |
Silva | Parametric design, aerodynamic analysis and parametric optimization of a solar UAV | |
Chopra | Small UAS and delivery drones: Challenges and opportunities the 38th Alexander A. Nikolsky honorary lecture | |
Gyllhem et al. | Numerical simulation of flow around the Colorado Micro Aerial Vehicle | |
Makgantai et al. | Design optimization of wingtip devices to reduce induced drag on fixed-wings | |
Diaz et al. | Computational Analysis of Urban Air Mobility Vehicles |