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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.


Wing Optimization (1) 97%

Airfoil Optimization Select New Airfoil Midterm Ressults:


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.


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:


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.


rapport (1) 42%

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