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What Is Active Aeroelastic Wing
The X-53 Active Aeroelastic Wing (AAW) development program is an American research project that has been completed. This project was carried out jointly by the Air Force Research Laboratory (AFRL), Boeing Phantom Works, and NASA's Dryden Flight Research Center. At NASA's Dryden Flight Research Center, the technology was flight tested on a modified McDonnell Douglas F/A-18 Hornet. Active Aeroelastic Wing Technology is a technology that blends the aerodynamics, controls, and structure of a wing in order to harness and regulate the aeroelastic twist that a wing experiences under dynamic stresses and high speeds. The use of multiple leading and trailing edge controls, such as "aerodynamic tabs," enables subtle amounts of aeroelastic twist to be controlled to provide large amounts of wing control power, while simultaneously minimizing maneuver air loads under high wing strain conditions or aerodynamic drag under low wing strain conditions. This is accomplished while maintaining a balance between the two extremes of wing strain conditions. This operation served as the very first demonstration of AAW technology on a large scale.
How You Will Benefit
(I) Insights, and validations about the following topics:
Chapter 1: Active Aeroelastic Wing
Chapter 2: Aileron
Chapter 3: Aeroelasticity
Chapter 4: Elevon
Chapter 5: NASA X-43
Chapter 6: List of experimental aircraft
Chapter 7: Boeing X-45
Chapter 8: Grumman X-29
Chapter 9: Air Force Research Laboratory
Chapter 10: Boeing X-48
Chapter 11: Elevator (aeronautics)
Chapter 12: Flap (aeronautics)
Chapter 13: United States Air Force Stability and Control Digital DATCOM
Chapter 14: Leading-edge cuff
Chapter 15: Flaperon
Chapter 16: Spoileron
Chapter 17: McDonnell Douglas F-15 STOL/MTD
Chapter 18: Boeing X-51 Waverider
Chapter 19: Adaptive compliant wing
Chapter 20: Leading-edge slat
Chapter 21: General Dynamics-Boeing AFTI/F-111A Aardvark
(II) Answering the public top questions about boeing x53 active aeroelastic wing.
(III) Real world examples for the usage of boeing x53 active aeroelastic wing in many fields.
(IV) 17 appendices to explain, briefly, 266 emerging technologies in each industry to have 360-degree full understanding of boeing x53 active aeroelastic wing' technologies.
Who This Book Is For
Professionals, undergraduate and graduate students, enthusiasts, hobbyists, and those who want to go beyond basic knowledge or information for any kind of boeing x53 active aeroelastic wing.
The X-53 Active Aeroelastic Wing (AAW) development program is an American research project that has been completed. This project was carried out jointly by the Air Force Research Laboratory (AFRL), Boeing Phantom Works, and NASA's Dryden Flight Research Center. At NASA's Dryden Flight Research Center, the technology was flight tested on a modified McDonnell Douglas F/A-18 Hornet. Active Aeroelastic Wing Technology is a technology that blends the aerodynamics, controls, and structure of a wing in order to harness and regulate the aeroelastic twist that a wing experiences under dynamic stresses and high speeds. The use of multiple leading and trailing edge controls, such as "aerodynamic tabs," enables subtle amounts of aeroelastic twist to be controlled to provide large amounts of wing control power, while simultaneously minimizing maneuver air loads under high wing strain conditions or aerodynamic drag under low wing strain conditions. This is accomplished while maintaining a balance between the two extremes of wing strain conditions. This operation served as the very first demonstration of AAW technology on a large scale.
How You Will Benefit
(I) Insights, and validations about the following topics:
Chapter 1: Active Aeroelastic Wing
Chapter 2: Aileron
Chapter 3: Aeroelasticity
Chapter 4: Elevon
Chapter 5: NASA X-43
Chapter 6: List of experimental aircraft
Chapter 7: Boeing X-45
Chapter 8: Grumman X-29
Chapter 9: Air Force Research Laboratory
Chapter 10: Boeing X-48
Chapter 11: Elevator (aeronautics)
Chapter 12: Flap (aeronautics)
Chapter 13: United States Air Force Stability and Control Digital DATCOM
Chapter 14: Leading-edge cuff
Chapter 15: Flaperon
Chapter 16: Spoileron
Chapter 17: McDonnell Douglas F-15 STOL/MTD
Chapter 18: Boeing X-51 Waverider
Chapter 19: Adaptive compliant wing
Chapter 20: Leading-edge slat
Chapter 21: General Dynamics-Boeing AFTI/F-111A Aardvark
(II) Answering the public top questions about boeing x53 active aeroelastic wing.
(III) Real world examples for the usage of boeing x53 active aeroelastic wing in many fields.
(IV) 17 appendices to explain, briefly, 266 emerging technologies in each industry to have 360-degree full understanding of boeing x53 active aeroelastic wing' technologies.
Who This Book Is For
Professionals, undergraduate and graduate students, enthusiasts, hobbyists, and those who want to go beyond basic knowledge or information for any kind of boeing x53 active aeroelastic wing.