09 Jun uestion Research Paper Swept Wing Aerodynamics (Concorde)
uestion
Research Paper Swept Wing Aerodynamics (Concorde)
Must use annotated bibliography to best of ability (attached)
Write a 4–6-page research paper on the unique aerodynamic characteristics of swept wing aerodynamics. Your paper should not discuss the capabilities of the aircraft unless these capabilities pertain to the aircraft’s unique aerodynamic design. The topics addressed in the Dole text provide specific aerodynamic areas to address as they relate to your chosen aircraft. Unique characteristics might include:
Airfoils and aerodynamic forces: unique airfoil design to enhance the airfoil’s purpose (speed, lift, etc.)
Lift/Drag: the relationship that lift and drag have to each other and the design characteristics to optimize each
Jet Aircraft/Propeller Aircraft: similarities and differences and their use in commercial/military/missions aviation
Slow-speed flight: how design enhances both performance and safety
Maneuvering Performance: maneuverability/controllability relationship and its effect on aircraft design
Longitudinal, directional, and lateral stability and control: the relationship between each during typical phases of flight
High-speed flight: those aspects unique to airframe, engine performance, and the challenges of flight from takeoff to landing
The paper must adhere to current APA formatting and include a title page, abstract, and reference page (none of which are included in the page count). A minimum of 3 sources must be used, only 2 of which can be from non-academic websites. Do not use Wiki sites. The other sources must be academic, scholarly resources.
Annotated Bibliography
Küchemann, Dietmar. (2012). Aerodynamic Design of Aircraft. American Institute of Aeronautics and Astronautics. Retrieved from https://app.knovel.com/hotlink/toc/id:kpADA0000T/aerodynamic-design-aircraft/aerodynamic-design-aircraft
· This book is primarily focused around the Concorde aircraft. It goes into detail of the design of swept aircraft as well as how this wing generates lift. The treatment of airflow is discussed as well as the means of generating lift. It describes the properties of slender aircraft and compares to properties of design of classical aircraft versus swept aircraft. It also goes into detail about propulsive forces and the properties in design of supersonic aircraft.
Dole, Charles E. Lewis, James E. Badick, Joseph R. Johnson, Brian A.. (2017). Flight Theory and Aerodynamics – A Practical Guide for Operational Safety (3rd Edition). John Wiley & Sons.
· This book goes into detail about stalls in swept wing aircraft. It also details the stall patterns and compares straight wing aircraft versus swept wing aircraft stall characteristics. There is also detail on the effects of swept wings during subsonic flight and why straight wings are not beneficial for this type of flight.
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