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Lecture notes

Aerodynamics Lecture 5

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The 5th lecture on Aerodynamics for 1st year Aeronautical Engieering students at Imperial College London covering the foundations of the subjects in depth and in detail

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A101 Introduction to Aerodynamics Section 1-5
__________________________________________________________________________
Outline
• We have previously considered a control volume when considering the conservation of
mass.
• We have also introduced/reviewed partial differentiation.
• Today we will use both these ideas to form the basic equation governing hydrostatics
• Whilst you may be familiar with the results from your previous studies try and follow the
form of the formulation since we will re-use these ideas in deriving the governing
equations of conservation of mass and momentum.

Hydrostatics

There is no motion of the fluid to consider.

Z

Although we typically use ‘y’ as the vertical
coordinate we shall use adopt the convention of
using ‘z’ in our discussion of hydrostatics since
this is the normal convention




yl
I


Therefore consider the forces on a control volume in a fluid in which the
pressure only varies with ‘z’, i.e. P=P(z).


P2 Ga)
' 1111
-
baby
wt b-
! Eddy
(
weight) f ← son




G)
P1



We want to determine the force balance between the pressure acting on the control volume
and the weight of the mass in the control volume.



1

, A101 Introduction to Aerodynamics Section 1-5
__________________________________________________________________________
Vertical force acting on control volume due to pressure.

= Area Lover Area
Upper pressure x -




pressure x


= - P2 ΔxΔy + P1 ΔxΔy

= -


( Pa + Pi ) Doody
=
D
Doody
-




p
This force must be balanced by the weight of the fluid in the control volume, i.e. W = mg
where, g, is the acceleration due to gravity. Therefore the force due to gravity (which acts
downwards)



pbxbybzg
-W= -mg = -




Net force = 0 = Force on CV due to pressure + Force on CV due to weight


Dp doc by Doody bag
=
p
-
-




O =
Dada
-




pg
-




Taking the limit as Δz →0 we obtain

dp
= − ρg (1)
dz

If we know how ρ varies with ‘z’ and g is a constant then we can integrate this equation.

Z constant
pg
For example if ρ = constant then P = -



t

Or
P constant
pg
z
-

t -




Pg 6)
z
Pat
h -

p a

pgh =




P
Pa
pgh
- -


-




0 P=Pa


If P = Pa at z = 0 then at z = h we have




2

Connected book
 image
John David Anderson Fundamentals of Aerodynamics
Publisher: 2016 ISBN: 9781259251344 Edition: Unknown

Document information

Study
Unknown
Uploaded on
August 23, 2022
Number of pages
5
Written in
2022/2023
Type
Lecture notes
Professor(s)
Dr sherwin
Contains
Lecture 3
£6.99

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