ES 202 Fluid and Thermal Systems Lecture 29: Drag and Lift Coefficients (2/18/2003) - PowerPoint PPT Presentation

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ES 202 Fluid and Thermal Systems Lecture 29: Drag and Lift Coefficients (2/18/2003)

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effects of body shape on drag (blunt body versus slender body) ... recognize blunt body geometry. pressure drag as dominant drag component ... – PowerPoint PPT presentation

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Title: ES 202 Fluid and Thermal Systems Lecture 29: Drag and Lift Coefficients (2/18/2003)


1
ES 202Fluid and Thermal SystemsLecture
29Drag and Lift Coefficients(2/18/2003)
2
Assignments
  • Homework
  • 13-56C, 13-62, 13-63, 13-72C, 13-88
  • Reading
  • 13-7 to 13-8

3
Announcements
  • Guest speaker Dr. John Adams will talk 2 talks
    today
  • Hypersonic Systems, Technology, and Testing,
    including relevant remarks on the recent Columbia
    Space Shuttle tragedy in O259 at 420 pm
  • Flight Mechanics of a Spinning Dimpled Spheroid
    in the Khan Room at 600 pm
  • Homework assigned this week is just for your
    learning, no need to hand it in

4
Road Map of Lecture 29
  • Finish up example on drag coefficient of
    cross-flow cylinder in a wind tunnel
  • Give out answers to in-class drag analyses
    yesterday
  • Introduce definition of drag coefficients
  • (Combined) Drag coefficients for objects of
    various geometries
  • concept of streamlining
  • Categorization of drag components
  • skin frictional drag versus pressure drag
  • effects of body shape on drag (blunt body versus
    slender body)
  • flow separation (an artifact of fluid viscosity)
  • Exercise on qualitative description of flow
    acceleration and pressure variation over a blunt
    body
  • notion of stagnation point (high pressure)
  • Applications
  • truck tipping problem

5
Answers to Drag Analyses
  • Drag analysis on a flat plate
  • Drag analysis on a cross-flow cylinder in open
    air
  • Drag analysis on a cross-flow cylinder in a wind
    tunnel

6
Drag Coefficient
  • From the results of drag analysis on a cross-flow
    cylinder in open air,
  • a non-dimensional group, the drag coefficient CD
    , can be defined
  • The definition of drag coefficient can also be
    arrived by means of dimensional analysis, similar
    to that on boundary layer thickness.
  • Show drag coefficient tables for various
    geometries

7
Categorization of Drag Components
  • The total drag force on an object can be broadly
    classified into two categories

Total drag force
  • Friction drag
  • directly related to
  • skin friction on surfaces
  • dominant on slender bodies
  • Pressure (form) drag
  • indirectly related to fluid viscosity
  • due to momentum losses through viscosity
  • mostly involves flow separation
  • dominant on blunt bodies
  • Relative importance between friction drag and
    pressure drag is strongly Reynolds number
    dependent and geometry dependent (slender versus
    blunt bodies).

8
Fluid Acceleration and Pressure Variation
  • Perform a qualitative assessment on the changes
    in a flow as it approaches a blunt object.
  • speed decreases, pressure increases from
    free-stream to stagnation point
  • highest pressure at stagnation point
  • flow splits into upper and lower streams
  • speed increases, pressure decreases from
    stagnation point to edges
  • highest speed and lowest pressure at the edges
  • flow speed decreases and pressure recovers behind
    the object
  • too much momentum loss in boundary layer not
    enough momentum to negotiate pressure hill, flow
    separates
  • large pressure difference between front and back
    sides causes pressure drag

9
Example Problem
  • Truck tipping problem
  • recognize blunt body geometry
  • pressure drag as dominant drag component
  • moment analysis about Point O to determine
    minimum wind speed to tip truck
  • assume drag coefficient is all attributed to
    pressure drag
  • assume line of action of pressure drag to be at
    the geometrical center of truck
  • at tipping position, R2 0
  • fine points
  • small frictional drag component in tabulated CD
    value
  • asymmetry in problem not accounted for in
    tabulated CD value

10
Terminal Speed of Falling Objects
  • Identify the major forces on a falling object
  • As the falling object accelerates, the drag force
    increases rapidly (quadratic dependence on
    falling speed).
  • At terminal speed, the net force on the falling
    object is zero, implying a perfect balance
    between body weight and drag.
  • The force balance sets the condition to determine
    the terminal speed.
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