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project1 100%

MAE 551, Airfoil Theory Project 1 Problem 1 (100 points) You have been called on to design a low-drag fairing for a UAV.

https://www.pdf-archive.com/2017/10/05/project1/

05/10/2017 www.pdf-archive.com

Wing Optimization (1) 97%

Airfoil Optimization Select New Airfoil Midterm Ressults:

https://www.pdf-archive.com/2018/10/18/wingoptimization-1/

18/10/2018 www.pdf-archive.com

Specifications 95%

Features and benefits • Patented airfoil system includes six airfoils and cuffed winglets that maximize performance and efficiency • Industrial-grade motor and gearbox offers efficient, reliable and durable operation • Weighs less than 145 lb (65.8 kg) allowing for easy positioning and installation • Factory-wired motor and controller cable with optional power cord plug • Perfect for spaces up to 70 x 70-ft (21.3 x 21.3-m) and ceilings as low as 14-ft (4.3-m) • Year-round energy savings, up to 10° cooling effect in hot weather and 1% energy savings per foot of ceiling height in cold weather The unique aerodynamic design enhances both energy efficiency and airflow by eliminating vortex formation at the airfoil tips.

https://www.pdf-archive.com/2016/06/24/specifications/

24/06/2016 www.pdf-archive.com

Carson Haack Resume edit 56%

Wing and Airfoil Theory, Engineering Optimization, Aircraft Systems, Theory of Elasticity ACADEMIC AND PROFESSIONAL EXPERIENCE Research Assistant, University of Alabama Department of Aerospace Engineering and Mechanics March 2014-Present “Developing a Damping Model using Fractional Calculus”  Objective:

https://www.pdf-archive.com/2016/02/18/carson-haack-resume-edit/

18/02/2016 www.pdf-archive.com

midterm comp 50%

The interaction between the air and the compressor blades are analyzed via diagrams known as velocity triangles, which show the relative and absolute air speeds based on airfoil geometry.

https://www.pdf-archive.com/2015/10/15/midterm-comp/

15/10/2015 www.pdf-archive.com

rapport (1) 42%

Below is a mesh generated with FreeFem for a NACA0012 airfoil inside a wind tunnel.

https://www.pdf-archive.com/2015/11/02/rapport-1/

02/11/2015 www.pdf-archive.com