Essays about: "high angle of attack"
Showing result 1 - 5 of 14 essays containing the words high angle of attack.
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1. Wake analysis for NACA4412 in free-flight condition
University essay from KTH/Skolan för teknikvetenskap (SCI)Abstract : The purpose of this project is to evaluate the differences in the wake of a NACA 4412 airfoil in free-flight condition compared to wind tunnel and also investigate wall-interference. This was done using two sets of angles of attack, 5 degrees and 8 degrees. READ MORE
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2. Numerical Study on Aerodynamic Drag Reduction on a Rear Wing of a Formula Student Car
University essay from KTH/Skolan för teknikvetenskap (SCI)Abstract : The importance of aerodynamics in racing has increased substantially over the past decades. Racing vehicles utilize different aerodynamic devices, to redirect the airflow around the vehicle in a beneficial way. The increase in downforce using an aerodynamic wing package increases drag force. READ MORE
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3. Vertical landing flight envelope definition
University essay from Luleå tekniska universitet/RymdteknikAbstract : This paper will investigate the development of a landing footprint for a re-entry vehicle. Vehicles can re-enter the atmosphere with a range of orientations, velocities and flight path angles. READ MORE
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4. Design of a drone system for maritime search and rescue missions
University essay from KTH/FlygdynamikAbstract : The work summarized in this report aims to investigate how a drone airplane design can be optimized to create a safer and more efficient sea rescue by providing staff with an early picture, performing search missions and aiding communication through visual contact. A flying wing is in theory one of the most efficient designs for a fixed wing aircraft, at the same time as it also offers high structural efficiency for its given size. READ MORE
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5. Enabling high-fidelity measurements of turbulent boundary layer flow over wing sections in the MTL wind tunnel.
University essay from KTH/MekanikAbstract : A reinforced fiber-glass model of a NACA 4412 wing profile is designed and set-up in the Minimum Turbulence Level (MTL) wind tunnel facility at KTH. The model has 65 pressure taps orifices, and the set-up includes two mounting panels designed to allow for particle image velocimetry (PIV) and hot wire anemometry (HWA) measurements of the boundary layer (to be performed in a future campaign). READ MORE