SPIE论文调研笔记

1、智能材料结构在飞行器上的应用SPIE论文调研笔记1. Wing Shaping for Optimum Roll PerformanceUsing Independent Modal-Space Control Technique Proceedings of SPIE Vol. 3984 (2000) 2. DESIGN OF AN OPTIMUM SMART WING TO ENHANCE ROLL PERFORMANCE March 1999 SPIE Vol. 3667Rolling Aircraft with Twisted Wings3. Design, fabrication a

2、nd testing of a new twist-active wing design March 1998 SPIE Vol.3329.Root-Twist Active Wing General Arrangement and During Final Assembly4. Comparison of smart-wing concepts for traflsonic cruise drag reductionSPIE Vol. 3044Adaptive-Wing ConceptTerfenol-Powered Smart Trailing EdgeSketch of a segmen

3、ted flap system for an airfoil5. Adaptive Smart Wing Design for Military Aircraft: Requirements, Concepts and Payoffs SPIE Vol. 2447Smart Wing Concepts and FeaturesAdaptive Wing Concepts and Features ComparisonTorque and Rotation Requirements（the F/A-18 aircraft）Actuation Rate RequirementsSmart Wing

4、 Design FeaturesWing Twist Activation ConceptsAntagonistic Actuation6. Adaptive wing structures Proceedings of SPIE Vol. 5388 (SPIE, Bellingham, WA, 2004)7. DARPA/AFRL/NASA Smart Wing Second Wind Tunnel Test ResultsMarch 1999 SPIE Vol. 3674 To quantify the benefits of smart materials and structures

5、adaptive wing technology, Northrop Grumman Corp. (NGC) built and tested two 16% scale wind tunnel models (a conventional and a smart model) of a fighter/attack aircraft under the DARPA/AFRL/NASA Smart Materials and Structures Development - Smart Wing Phase 1. Performance gains quantified included in

6、creased pitching moment (Cj, increased rolling moment (C,) and improved pressure distribution. The benefits were obtained for hingeless, contoured trailing edge control surfaces with embedded shape memory alloy (SMA) wires and spanwise wing twist effected by SMA torque tube mechanisms, compared to c

7、onventional hinged control surfaces.FLOW CHARACTERISTICS OVER HINGED ANDHINGELESS CONTOURED CONTROL SURFACES8. Design of Composite Smart Wing to Enhance Roll ManeuverSPIE Vol. 3321有限元模型9. Smart Wing Wind Tunnel Test Results SPIE VoL 3044SMART WING MODEL WITH DEFLECTED SMA FLAP10. Design of a shape-m

8、emory alloy actuated macro-scale morphing aircraft mechanism Proc. of SPIE Vol. 5764 (SPIE, Bellingham, WA, 2005)Component of COSMOS mesh and finite element stress results for SMA-driven11. Adaptive Wing Structures Proceedings of SPIE Vol. 5762 (SPIE, Bellingham, WA, 2005) Cut-out of cast, wing-shap

9、ed Veritex returning from rolled state12. Morphing Aircraft Concepts, Classifications, and ChallengesProceedings of SPIE Vol. 5388 (SPIE, Bellingham, WA, 2004)Classification of morphing aircraft technologyTechnical challenges encountered in the design of a morphing aircraft13. Application of Shape M

10、emory Alloy (SMA) Spars for Aircraft Maneuver Enhancement Proceedings of SPIE Vol. 4701 (2002)A modeled F-16 wing with nine SMA spar set14. Active Shape Airfoil Control through Composite-Piezoceramic Actuators Proceedings of SPIE Vol. 4327 (2001)Transonic aerodynamic field around the selected wing s

11、ection.Bump concept and actuators scheme.15. Development and design of flexible Fowler flaps for an adaptive wingSPIE Vol. 3326 Flexible Fowler flapsPosition and distribution of flexible ribs in the Fowler flapsGeometry of an elementDesign of upper and lower skin16. Adaptive flight controi surfaces,

12、 wings, rotors and active aerodynamics SPIE Vol. 2717Mass, Volume, Energy and Efficiency Comparison of Conventional and Adaptive Flight Control Actuator Systems over a Simulated 60 Sec. Flight of a FOG-M MissileProjected Time-Line of Active Flight Control ProjectsArrangement of CAP and DAP Twist-Act

13、ive LaminaSolid State Rotor System (SSRS) with Torque-Plate Pitch Actuators17. Missile ifight control using active flexspar actuators SPIE Vol. 2443Flexspar Missile Wing Internal StructureOne Third Scale TOW 2B Missile Model Mounted in Low Speed Wind Tunnel18. Modeling techniques and design principl

14、es of a low aspect ratio active aeroservoelastic wing SPIE Vol. 1917（1993）PROGRESSION OF HYPOTHETICAL CONTROL DEFLECTIONS AND RESULTING MISSILE ATTITUDE19. Design and application of compliant mechanisms for morphing aircraft structures Proceedings of SPIE Vol. 5054 (2003)Leading and trailing edge me

15、chanisms developed for the F-111 Mission Adaptive Wing program20. FINITE ELEMENT SIMULATION OF ADAPTIVE AEROSPACE STRUCTURES WITH SMA ACTUATORSProceedings of SPIE Vol. 5049 (2003)“Smart Wing” concepts21. Development of High-Rate, Large Deflection, Hingeless Trailing Edge Control Surface for the Smart Wing Wind Tunnel ModelProceedings of SPIE Vol. 4332 (2001)Distributed Moment Concept With Actively Cooled Antagonistic SMA Wires22. Materials and actuators for the shape control of structuresProceedings of SPIE Vol. 4327 (2001)main properties of various