MY 3241
MY 3241 - Benjamin Franklin Institute Of Technology Study Resources
  • 6 Pages matlab streamfunction examples
    Matlab Streamfunction Examples

    School: Benjamin Franklin Institute Of Technology

  • 3 Pages MAE 3241 Hmk1 Solution
    MAE 3241 Hmk1 Solution

    School: Benjamin Franklin Institute Of Technology

  • 1 Page MAE 3241 Hmk 5
    MAE 3241 Hmk 5

    School: Benjamin Franklin Institute Of Technology

    MAE 3241: Aerodynamics and Flight Mechanics Homework #5 Assigned: March 16, 2007 Due: March 26, 2007 Question 1: Consider an infinite wing with an NACA 1412 airfoil section and a chord length of 3 ft. The wing is at an angle of attack of 5 in an ai

  • 59 Pages 3241 Lecture 19
    3241 Lecture 19

    School: Benjamin Franklin Institute Of Technology

    MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS REVIEW OF INCOMPRESSIBLE FLOW OVER AIRFOILS AND WINGS Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk AIRFOILS VERSUS WINGS Why do airfoils have such a shape? H

  • 1 Page 3241.CQ11
    3241.CQ11

    School: Benjamin Franklin Institute Of Technology

    MAE 3241: Aerodynamics and Flight Mechanics Concept Quiz #11 Name: _ Consider a rectangular wing with an NACA 0009 airfoil spanning the test section of a wind tunnel (we say spanning the entire test section to indicate that the wing has no ends, or

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