Predictive Methods for the Dynamic Response of a Quad Tilt-duct V/STOL Aircraft in Transition PDF Download
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Author: Irving Carl Statler
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 466
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Book Description
Author: Irving Carl Statler
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 466
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Book Description
Author: George Kurylowich
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 212
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Book Description
An analysis was performed to investigate the longitudinal stability and control characteristics of an ejector wing configuration V/STOL in transition. A derivative approach was used to obtain dynamic responses about specified trim speeds, and analysis of these responses provided an insight into the significant characteristics that might affect the pilot's control over the aircraft. The thrust levels necessary to meet the control requirements specified in MIL-F-83300 for a Level 1 category vehicle were determined as well. A similar study was made for a stowable rotor configuration, and results for the stowable rotor V/STOL and the ejector wing configuration were compared. Finally, the downwash characteristics of the ejector wing configuration were evaluated in terms of their effect on ground equipment and personnel. Spray generation during hover over water is also discussed.
Author: Hrishikesh Saha
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 874
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Book Description
Author:
Publisher:
ISBN:
Category : Ground-cushion phenomenon
Languages : en
Pages : 870
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Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1734
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Book Description
Author: George E. Cooper
Publisher:
ISBN:
Category : Air pilots
Languages : en
Pages : 60
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Book Description
Author:
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 1012
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Book Description
Author: James A. Franklin
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Mathematics
Languages : en
Pages : 240
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Book Description
Annotation This text presents the principles of dynamics and control for vertical, short take-off landing (V/STOL) aircraft. It is the first book of its kind. It is intended for graduate students and professionals in aeronautics who have knowledge of linear systems analysis, aircraft static, dynamic stability, and control. The text begins with a discussion of V/STOL aircraft operations. Control strategies, equations of motion, longitudinal and lateral-directional flying qualities in both hover and forward flight, wind and turbulence responses, and control augmentation and cockpit displays are covered. Specific examples of the YAV-8B Harrier and XV-15 Tilt Rotor aircraft are used to illustrate actual V/STOL dynamic and control characteristics.
Author:
Publisher:
ISBN:
Category : Nuclear science abstracts
Languages : en
Pages : 1000
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Book Description
Author: Kimon P. Valavanis
Publisher: Springer Science & Business Media
ISBN: 1402061145
Category : Technology & Engineering
Languages : en
Pages : 552
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Book Description
The past decade has seen tremendous interest in the production and refinement of unmanned aerial vehicles, both fixed-wing, such as airplanes and rotary-wing, such as helicopters and vertical takeoff and landing vehicles. This book provides a diversified survey of research and development on small and miniature unmanned aerial vehicles of both fixed and rotary wing designs. From historical background to proposed new applications, this is the most comprehensive reference yet.
