Computer Networking: A Top-Down Approach (7th Edition)
Computer Networking: A Top-Down Approach (7th Edition)
7th Edition
ISBN: 9780133594140
Author: James Kurose, Keith Ross
Publisher: PEARSON
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Task 3
def print_table(
values: tuple [float, ...], drag_coeff: float, increments: int, step: float
) -> None:
Parameters:
values (tuple [float, ...]): mass, force, ref_area, density,
init_velocity, lift_velocity, start_position, time_inc
drag_coeff (float): The drag coefficient.
increments (int): The number of drag coefficients displayed.
step (float): The difference between each drag coefficient.
10
11
12
Returns:
13
None
14
15
For this function you need to compute the distance before lift-off for a range of drag coefficients
and then you need to print these results in a table.
The drag coefficient of an aeroplane has a significant impact on the plane's ability to lift-off. If the
drag coefficient is sufficiently high, the plane will not actually be able to generate enough speed to
lift off. In this task you will write a function which will explore this phenomenon.
Example
>>> values - (50000.0, 600000.0, 800.0, 1.0, 0.0, 70.0, 0.0, 0.1)
>>> drag_coeff - 0.015
>>> print_table(values, drag_coeff, 10, 0.03)
...
• Drag coefficient • Runway distance •
0.015
214.218
0.045
224.707
0.075
234.859
0.105
251.633
0.135
267.901
0.165
297.560
0.195
326.334
0.225
367.907
0.255
435.575
0.285
583.499
Hint: You should create the above table by using f-string formatting. Check the appendix for layout
dimensions.
expand button
Transcribed Image Text:Task 3 def print_table( values: tuple [float, ...], drag_coeff: float, increments: int, step: float ) -> None: Parameters: values (tuple [float, ...]): mass, force, ref_area, density, init_velocity, lift_velocity, start_position, time_inc drag_coeff (float): The drag coefficient. increments (int): The number of drag coefficients displayed. step (float): The difference between each drag coefficient. 10 11 12 Returns: 13 None 14 15 For this function you need to compute the distance before lift-off for a range of drag coefficients and then you need to print these results in a table. The drag coefficient of an aeroplane has a significant impact on the plane's ability to lift-off. If the drag coefficient is sufficiently high, the plane will not actually be able to generate enough speed to lift off. In this task you will write a function which will explore this phenomenon. Example >>> values - (50000.0, 600000.0, 800.0, 1.0, 0.0, 70.0, 0.0, 0.1) >>> drag_coeff - 0.015 >>> print_table(values, drag_coeff, 10, 0.03) ... • Drag coefficient • Runway distance • 0.015 214.218 0.045 224.707 0.075 234.859 0.105 251.633 0.135 267.901 0.165 297.560 0.195 326.334 0.225 367.907 0.255 435.575 0.285 583.499 Hint: You should create the above table by using f-string formatting. Check the appendix for layout dimensions.
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