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A First Course in Linear Algebra, 2017a

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1.2. Systems of Equations, <strong>Algebra</strong>ic Procedures 35<br />

The solution is given by<br />

which can be written as<br />

x − w = 0<br />

y − 1 3 w = 0<br />

z − 1 3 w = 0<br />

x = t<br />

y = 1 3 t<br />

z = 1 3 t<br />

w = t<br />

Choose a value for t, say 3. Then w = 3 and this yields x = 3,y = 1,z = 1. It follows that the balanced<br />

reaction is given by<br />

3KOH + 1H 3 PO 4 → 1K 3 PO 4 + 3H 2 O<br />

Note that this results <strong>in</strong> the same number of atoms on both sides.<br />

Of course these numbers you are f<strong>in</strong>d<strong>in</strong>g would typically be the number of moles of the molecules on<br />

each side. Thus three moles of KOH added to one mole of H 3 PO 4 yields one mole of K 3 PO 4 and three<br />

moles of H 2 O.<br />

♠<br />

1.2.6 Dimensionless Variables<br />

This section shows how solv<strong>in</strong>g systems of equations can be used to determ<strong>in</strong>e appropriate dimensionless<br />

variables. It is only an <strong>in</strong>troduction to this topic and considers a specific example of a simple airplane<br />

w<strong>in</strong>g shown below. We assume for simplicity that it is a flat plane at an angle to the w<strong>in</strong>d which is blow<strong>in</strong>g<br />

aga<strong>in</strong>st it with speed V as shown.<br />

V<br />

θ<br />

A<br />

B<br />

The angle θ is called the angle of <strong>in</strong>cidence, B is the span of the w<strong>in</strong>g and A is called the chord.<br />

Denote by l the lift. Then this should depend on various quantities like θ,V ,B,A and so forth. Here is a<br />

table which <strong>in</strong>dicates various quantities on which it is reasonable to expect l to depend.<br />

Variable Symbol Units<br />

chord A m<br />

span B m<br />

angle <strong>in</strong>cidence θ m 0 kg 0 sec 0<br />

speed of w<strong>in</strong>d V msec −1<br />

speed of sound V 0 msec −1<br />

density of air ρ kgm −3<br />

viscosity μ kgsec −1 m −1<br />

lift l kgsec −2 m

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