MY 3241  Benjamin Franklin Institute Of Technology Study Resources

Matlab Streamfunction Examples
School: Benjamin Franklin Institute Of Technology

3241 Lecture 10
School: Benjamin Franklin Institute Of Technology
MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS Introduction to Streamlines, Stream Functions, and Velocity Potential February 2, 2007 Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk WHAT DOES EULER'S EQUATION

3241.CQ5 Solution
School: Benjamin Franklin Institute Of Technology
3241: Aerodynamics and Flight Mechanics Name: _Solution_ Concept Quiz #5 Consider again the example of the rocket on a thrust stand discussed in class. An actual rocket in flight is not attached to a thrust stand and is free to rapidly accelerate t

3241.CQ4
School: Benjamin Franklin Institute Of Technology
3241: Aerodynamics and Flight Mechanics Concept Quiz #4 Name: _ The purpose of this concept quiz is to examine the application momentum equation for part of a control surface analysis. The momentum equation is: d d d d d ^ UdV + U (U n)dS = F d

3241.CQ2 Solution
School: Benjamin Franklin Institute Of Technology

3241.CQ2
School: Benjamin Franklin Institute Of Technology
MAE 3241: Aerodynamics and Flight Mechanics Concept Quiz #2 Name: _ A two dimensional flow field is observed to have the following components: u = a x2  y2 ( ) v = 2axy w=0 Is this flow incompressible? Is this flow irrotational?

3241 Lecture 4
School: Benjamin Franklin Institute Of Technology
MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS Views of Motion: Eulerian and Lagrangian January 22, 2007 Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk VECTOR CALCULUS REVIEW ( a ) = 0 The curl of the gra

3241 Lecture 3
School: Benjamin Franklin Institute Of Technology
MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS Review of Fundamental Definitions and Examples January 19, 2007 Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk Spring 2007 WHAT CREATES AERODYNAMIC FORCES? Aer

MAE 3241 Hmk1 Solution
School: Benjamin Franklin Institute Of Technology

3241.CQ1 Solution
School: Benjamin Franklin Institute Of Technology
MAE 3241: Aerodynamics and Flight Mechanics Concept Quiz #1 Circle all the answer choices that apply: Name: _ 1. My primary area of interest within aerospace engineering is (structures / aerodynamics / flight controls / propulsion). 2. As a future

3241 Final Review
School: Benjamin Franklin Institute Of Technology
MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS Final Exam Review and Closing Comments Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk OVERVIEW OF ACCOMPLISHMENT "This book is designed for a 1year course in

MATLAB Tutorial
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3241 Lecture 39
School: Benjamin Franklin Institute Of Technology
MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS Compressible Flow Over Airfoils: Linearized Subsonic Flow April 23, 2007 Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk WHAT ARE WE DOING NOW? Goal: Examine

3241 Syllabus 2007
School: Benjamin Franklin Institute Of Technology
MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS Spring 2007 Course Website: http:/my.fit.edu/~dkirk/3241 Daniel R. Kirk Email: dkirk@fit.edu Phone: (321) 6747622 Office: Olin Engineering Center 215 Office Hours: Tuesday 911 am and Thursday 24 pm Lectu

Dihedral
School: Benjamin Franklin Institute Of Technology
MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS Examples of Dihedral, Anhedral, Adverse Yaw and Leading Edge Extensions April 11, 2007 Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk DIHEDRAL Dihedral, , is

3241.CQ13
School: Benjamin Franklin Institute Of Technology
MAE 3241: Aerodynamics and Flight Mechanics Concept Quiz #13 Name: _ A new airfoil design is given by 3 algebraic equations that provide an expression for the mean camber line (z/c) defined in terms of distance along the chord (x/c). Equation 1 is

MAE 3241 Hmk6 Solution
School: Benjamin Franklin Institute Of Technology

MAE 3241 Hmk 6
School: Benjamin Franklin Institute Of Technology
MAE 3241: Aerodynamics and Flight Mechanics Homework #6 Assigned: March 21, 2007 Due: March 30, 2007 Complete the following problems from the Fundamentals of Aerodynamics, 3rd Edition: 4.6 4.7 4.8 4.10 Also complete the following questions: Questio

3241.CQ12
School: Benjamin Franklin Institute Of Technology
MAE 3241: Aerodynamics and Flight Mechanics Concept Quiz #12 Name: _ Consider a thin, symmetric airfoil at 2 angle of attack. From the results of thin airfoil theory, calculate the lift coefficient and the moment coefficient about the leading edge.

TAFT
School: Benjamin Franklin Institute Of Technology
MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS Thin Airfoil Theory Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk OVERVIEW: THIN AIRFOIL THEORY Fundamental Equation of Thin Airfoil Theory : 1 ( ) d dz

MAE 3241 Hmk5 Solution
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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

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

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

MAE 3241 Hmk 4
School: Benjamin Franklin Institute Of Technology
MAE 3241: Aerodynamics and Flight Mechanics Homework #4 Assigned: February 21, 2007 Due: March 2, 2007 Complete the following problems from the Fundamentals of Aerodynamics, 4th Edition: 3.11 3.12 3.15 Also complete the following questions: Questio

3241 Exam 1
School: Benjamin Franklin Institute Of Technology
MAE 3241: Aerodynamics and Flight Mechanics February 11, 2005 Name: _ Exam #1 Exam is worth 100 points and has 4 questions (30/30/25/25). Read each question carefully and show all your work. Question 1 (30 Points): An F4 Phantom is being refueled

3241.CQ10 Solution
School: Benjamin Franklin Institute Of Technology

3241.CQ9
School: Benjamin Franklin Institute Of Technology
MAE 3241: Aerodynamics and Flight Mechanics Concept Quiz #9 Name: _ The Figure below (Figure 3.23 from Anderson) shows the superposition of a uniform flow and a sourcesink pair, which describes the flow over the socalled Rankine oval. We have sh

MAE 3241 Hmk 3
School: Benjamin Franklin Institute Of Technology
MAE 3241: Aerodynamics and Flight Mechanics Homework #3 Assigned: February 5, 2007 Due: February 14, 2007 Complete the following problems from the Fundamentals of Aerodynamics, 4th Edition: 1.11 1.13 2.7 Comment: For part (a) of this question, whic

3241.CQ7
School: Benjamin Franklin Institute Of Technology
MAE 3241: Aerodynamics and Flight Mechanics Concept Quiz #7 Name: _ A two dimensional, incompressible flow field is given by the velocity field: ^ V = 3 yi + 2 x^ j Does this flow field satisfy continuity? 1 If so, find the stream function (x,y) a