Sketch/idea of proof via the Law of Cosines: if \mathbf{w} = \mathbf{u} - \mathbf{v}, then∣ w ∣ 2 = ∣ u ∣ 2 + ∣ v ∣ 2 − 2 ∣ u ∣ ∣ v ∣ cos θ , |\mathbf{w}|^2 = |\mathbf{u}|^2 + |\mathbf{v}|^2 - 2 |\mathbf{u}| |\mathbf{v}| \cos \theta, ∣ w ∣ 2 = ∣ u ∣ 2 + ∣ v ∣ 2 − 2∣ u ∣∣ v ∣ cos θ , and since \mathbf{w} = \mathbf{u} - \mathbf{v}, \mathbf{w}\cdot \mathbf{w} = (\mathbf{u} - \mathbf{v}) \cdot (\mathbf{u} - \mathbf{v}) = |\mathbf{u}|^2 + |\mathbf{v}|^2 - 2 (\mathbf{u} \cdot \mathbf{v}).< / p > < / l i > < l i > < p > E q u a t i n g t h e t w o e x p r e s s i o n s a n d s i m p l i f y i n g y i e l d s < b r > </p></li><li><p>Equating the two expressions and simplifying yields<br> < / p >< / l i >< l i >< p > E q u a t in g t h e tw oe x p r ess i o n s an d s im pl i f y in g y i e l d s < b r > \cos \theta = \frac{\mathbf{u} \cdot \mathbf{v}}{|\mathbf{u}| |\mathbf{v}|}. < / p > < / l i > < / u l > < / l i > < l i > < p > K e y e x a m p l e c o m p u t a t i o n s ( i l l u s t r a t i v e ; v a l u e s m a y r e f l e c t t h e t r a n s c r i p t o r s t a n d a r d p r a c t i c e ) : < / p > < u l > < l i > < p > E x a m p l e 1 ( 3 D d o t p r o d u c t ) : < / p > < / l i > < l i > < p > C o m p u t e </p></li></ul></li><li><p>Key example computations (illustrative; values may reflect the transcript or standard practice):</p><ul><li><p>Example 1 (3D dot product):</p></li><li><p>Compute < / p >< / l i >< / u l >< / l i >< l i >< p > K ey e x am pl eco m p u t a t i o n s ( i l l u s t r a t i v e ; v a l u es ma y r e f l ec tt h e t r an scr i pt or s t an d a r d p r a c t i ce ) :< / p >< u l >< l i >< p > E x am pl e 1 ( 3 D d o tp r o d u c t ) :< / p >< / l i >< l i >< p > C o m p u t e (1, \, 2, \, -1) \cdot (-6, \, 2, \, -3) = (1)(-6) + (2)(2) + (-1)(-3) = -6 + 4 + 3 = 1. < / p > < / l i > < l i > < p > E x a m p l e 2 ( a n g l e b e t w e e n u = ( 1 , − 2 , − 2 ) a n d v = ( 6 , 3 , 2 ) ) : < / p > < / l i > < l i > < p > </p></li><li><p>Example 2 (angle between u = (1, -2, -2) and v = (6, 3, 2)):</p></li><li><p> < / p >< / l i >< l i >< p > E x am pl e 2 ( an g l e b e tw ee n u = ( 1 , − 2 , − 2 ) an d v = ( 6 , 3 , 2 )) :< / p >< / l i >< l i >< p > u \cdot v = 1\cdot 6 + (-2)\cdot 3 + (-2)\cdot 2 = 6 - 6 - 4 = -4. < / p > < / l i > < l i > < p > </p></li><li><p> < / p >< / l i >< l i >< p > |u| = \sqrt{1^2 + (-2)^2 + (-2)^2} = 3, \quad |v| = \sqrt{6^2 + 3^2 + 2^2} = 7. < / p > < / l i > < l i > < p > </p></li><li><p> < / p >< / l i >< l i >< p > \cos \theta = \frac{-4}{3 \cdot 7} = -\frac{4}{21} \approx -0.1905. < / p > < / l i > < l i > < p > </p></li><li><p> < / p >< / l i >< l i >< p > \theta \approx \cos^{-1}(-\frac{4}{21}) \approx 1.76 \text{ radians} \approx 100.98^ ext{\circ}. < / p > < / l i > < l i > < p > E x a m p l e 3 ( a n g l e i n t r i a n g l e w i t h A = ( 0 , 0 ) , B = ( 3 , 5 ) , C = ( 5 , 2 ) ) : < / p > < / l i > < l i > < p > V e c t o r s : C A → = ( − 5 , − 2 ) , C B → = ( − 2 , 3 ) . < / p > < / l i > < l i > < p > D o t : </p></li><li><p>Example 3 (angle in triangle with A=(0,0), B=(3,5), C=(5,2)):</p></li><li><p>Vectors: \overrightarrow{CA} = (-5, -2), \overrightarrow{CB} = (-2, 3).</p></li><li><p>Dot: < / p >< / l i >< l i >< p > E x am pl e 3 ( an g l e in t r ian g l e w i t h A = ( 0 , 0 ) , B = ( 3 , 5 ) , C = ( 5 , 2 )) :< / p >< / l i >< l i >< p > V ec t or s : C A = ( − 5 , − 2 ) , C B = ( − 2 , 3 ) . < / p >< / l i >< l i >< p > D o t : (-5)(-2) + (-2)(3) = 10 - 6 = 4. < / p > < / l i > < l i > < p > M a g n i t u d e s : </p></li><li><p>Magnitudes: < / p >< / l i >< l i >< p > M a g ni t u d es : |\overrightarrow{CA}| = \sqrt{29}, \quad |\overrightarrow{CB}| = \sqrt{13}. < / p > < / l i > < l i > < p > </p></li><li><p> < / p >< / l i >< l i >< p > \cos \theta = \frac{4}{\sqrt{29}\sqrt{13}} = \frac{4}{\sqrt{377}} \approx 0.206. < / p > < / l i > < l i > < p > </p></li><li><p> < / p >< / l i >< l i >< p > \theta \approx \cos^{-1}(0.206) \approx 1.36 \text{ radians} \approx 78.1^ ext{\circ}. < / p > < / l i > < / u l > < / l i > < l i > < p > O r t h o g o n a l i t y ( p e r p e n d i c u l a r v e c t o r s ) < / p > < u l > < l i > < p > D e f i n i t i o n : T w o n o n z e r o v e c t o r s a r e o r t h o g o n a l i f < b r > </p></li></ul></li><li><p>Orthogonality (perpendicular vectors)</p><ul><li><p>Definition: Two nonzero vectors are orthogonal if<br> < / p >< / l i >< / u l >< / l i >< l i >< p > O r t h o g o na l i t y ( p er p e n d i c u l a r v ec t or s ) < / p >< u l >< l i >< p > D e f ini t i o n : T w o n o n z er o v ec t or s a r eor t h o g o na l i f < b r > \mathbf{u} \cdot \mathbf{v} = 0. < / p > < / l i > < l i > < p > E x a m p l e s : < / p > < / l i > < l i > < p > ( a ) u = ( 3 , − 2 ) , v = ( 4 , 6 ) ⇒ u ⋅ v = 3 ⋅ 4 + ( − 2 ) ⋅ 6 = 12 − 12 = 0. </p></li><li><p>Examples:</p></li><li><p>(a) \mathbf{u} = (3, -2), \mathbf{v} = (4, 6) \Rightarrow \mathbf{u} \cdot \mathbf{v} = 3\cdot 4 + (-2)\cdot 6 = 12 - 12 = 0. < / p >< / l i >< l i >< p > E x am pl es :< / p >< / l i >< l i >< p > ( a ) u = ( 3 , − 2 ) , v = ( 4 , 6 ) ⇒ u ⋅ v = 3 ⋅ 4 + ( − 2 ) ⋅ 6 = 12 − 12 = 0.
(b) \mathbf{u} = (3, -2, 1), \mathbf{v} = (0, 2, 4) \Rightarrow \mathbf{u} \cdot \mathbf{v} = 0 + (-2)(2) + (1)(4) = 0. < / p > < / l i > < l i > < p > ( c ) T h e z e r o v e c t o r i s o r t h o g o n a l t o e v e r y v e c t o r : </p></li><li><p>(c) The zero vector is orthogonal to every vector: < / p >< / l i >< l i >< p > ( c ) T h ez er o v ec t or i sor t h o g o na l t oe v er y v ec t or : 0 \cdot \mathbf{u} = 0. < / p > < / l i > < / u l > < / l i > < l i > < p > D o t p r o d u c t p r o p e r t i e s ( a l g e b r a i c r u l e s ) < / p > < u l > < l i > < p > 1 ) C o m m u t a t i v i t y : </p></li></ul></li><li><p>Dot product properties (algebraic rules)</p><ul><li><p>1) Commutativity: < / p >< / l i >< / u l >< / l i >< l i >< p > D o tp r o d u c tp r o p er t i es ( a l g e b r ai cr u l es ) < / p >< u l >< l i >< p > 1 ) C o mm u t a t i v i t y : \mathbf{u} \cdot \mathbf{v} = \mathbf{v} \cdot \mathbf{u}. < / p > < / l i > < l i > < p > 2 ) S c a l a r c o m p a t i b i l i t y : </p></li><li><p>2) Scalar compatibility: < / p >< / l i >< l i >< p > 2 ) S c a l a r co m p a t ibi l i t y : (c\mathbf{u}) \cdot \mathbf{v} = c (\mathbf{u} \cdot \mathbf{v}) = \mathbf{u} \cdot (c\mathbf{v}). < / p > < / l i > < l i > < p > 3 ) D i s t r i b u t i v i t y : </p></li><li><p>3) Distributivity: < / p >< / l i >< l i >< p > 3 ) D i s t r ib u t i v i t y : (\mathbf{u} + \mathbf{w}) \cdot \mathbf{v} = \mathbf{u} \cdot \mathbf{v} + \mathbf{w} \cdot \mathbf{v}. < / p > < / l i > < l i > < p > 4 ) S e l f − d o t e q u a l s s q u a r e d m a g n i t u d e : </p></li><li><p>4) Self-dot equals squared magnitude: < / p >< / l i >< l i >< p > 4 ) S e l f − d o t e q u a l ss q u a r e d ma g ni t u d e : \mathbf{u} \cdot \mathbf{u} = |\mathbf{u}|^2. < / p > < / l i > < l i > < p > 5 ) Z e r o v e c t o r d o t p r o d u c t : </p></li><li><p>5) Zero vector dot product: < / p >< / l i >< l i >< p > 5 ) Z er o v ec t or d o tp r o d u c t : 0 \cdot \mathbf{u} = 0. < / p > < / l i > < l i > < p > S k e t c h o f p r o o f s ( s k e t c h e s o n l y ) : < / p > < / l i > < l i > < p > 1 ) B y e x p a n d i n g w i t h c o m p o n e n t s , t a k e u ⋅ v = u < e m > 1 v < / e m > 1 + u < e m > 2 v < / e m > 2 + u < e m > 3 v < / e m > 3 = v < e m > 1 u < / e m > 1 + v < e m > 2 u < / e m > 2 + v < e m > 3 u < / e m > 3 = v ⋅ u . < / p > < / l i > < l i > < p > 3 ) U s e l i n e a r i t y i n t h e f i r s t a r g u m e n t : u ⋅ ( v + w ) = u < e m > 1 ( v < / e m > 1 + w < e m > 1 ) + u < / e m > 2 ( v < e m > 2 + w < / e m > 2 ) + u < e m > 3 ( v < / e m > 3 + w 3 ) = u ⋅ v + u ⋅ w . < / p > < / l i > < / u l > < / l i > < l i > < p > V e c t o r p r o j e c t i o n a n d t h e s c a l a r c o m p o n e n t a l o n g a d i r e c t i o n < / p > < u l > < l i > < p > V e c t o r p r o j e c t i o n o f u o n t o a n o n z e r o v e c t o r v ( t h e c o m p o n e n t o f u i n t h e d i r e c t i o n o f v ) : < b r > </p></li><li><p>Sketch of proofs (sketches only):</p></li><li><p>1) By expanding with components, take \mathbf{u} \cdot \mathbf{v} = u<em>1 v</em>1 + u<em>2 v</em>2 + u<em>3 v</em>3 = v<em>1 u</em>1 + v<em>2 u</em>2 + v<em>3 u</em>3 = \mathbf{v} \cdot \mathbf{u}.</p></li><li><p>3) Use linearity in the first argument: \mathbf{u} \cdot (\mathbf{v} + \mathbf{w}) = u<em>1(v</em>1+w<em>1) + u</em>2(v<em>2+w</em>2) + u<em>3(v</em>3+w_3) = \mathbf{u} \cdot \mathbf{v} + \mathbf{u} \cdot \mathbf{w}.</p></li></ul></li><li><p>Vector projection and the scalar component along a direction</p><ul><li><p>Vector projection of \mathbf{u} onto a nonzero vector \mathbf{v} (the component of \mathbf{u} in the direction of \mathbf{v}):<br> < / p >< / l i >< l i >< p > S k e t c h o f p r oo f s ( s k e t c h eso n l y ) :< / p >< / l i >< l i >< p > 1 ) B y e x p an d in g w i t h co m p o n e n t s , t ak e u ⋅ v = u < e m > 1 v < / e m > 1 + u < e m > 2 v < / e m > 2 + u < e m > 3 v < / e m > 3 = v < e m > 1 u < / e m > 1 + v < e m > 2 u < / e m > 2 + v < e m > 3 u < / e m > 3 = v ⋅ u . < / p >< / l i >< l i >< p > 3 ) U se l in e a r i t y in t h e f i r s t a r g u m e n t : u ⋅ ( v + w ) = u < e m > 1 ( v < / e m > 1 + w < e m > 1 ) + u < / e m > 2 ( v < e m > 2 + w < / e m > 2 ) + u < e m > 3 ( v < / e m > 3 + w 3 ) = u ⋅ v + u ⋅ w . < / p >< / l i >< / u l >< / l i >< l i >< p > V ec t or p r o j ec t i o nan d t h esc a l a r co m p o n e n t a l o n g a d i r ec t i o n < / p >< u l >< l i >< p > V ec t or p r o j ec t i o n o f u o n t o an o n z er o v ec t or v ( t h eco m p o n e n t o f u in t h e d i r ec t i o n o f v ) :< b r > \text{proj}_{\mathbf{v}} \mathbf{u} = \left( \frac{\mathbf{u} \cdot \mathbf{v}}{\mathbf{v} \cdot \mathbf{v}} \right) \mathbf{v} = \left( \frac{\mathbf{u} \cdot \mathbf{v}}{|\mathbf{v}|^2} \right) \mathbf{v}. < / p > < / l i > < l i > < p > T h e u n i t d i r e c t i o n a l o n g v : t h e u n i t v e c t o r i s < b r > </p></li><li><p>The unit direction along \mathbf{v}: the unit vector is<br> < / p >< / l i >< l i >< p > T h e u ni t d i r ec t i o na l o n g v : t h e u ni t v ec t or i s < b r > \hat{\mathbf{v}} = \frac{\mathbf{v}}{|\mathbf{v}|}. < / p > < / l i > < l i > < p > S c a l a r c o m p o n e n t o f u i n t h e d i r e c t i o n o f v < b r > </p></li><li><p>Scalar component of \mathbf{u} in the direction of \mathbf{v}<br> < / p >< / l i >< l i >< p > S c a l a r co m p o n e n t o f u in t h e d i r ec t i o n o f v < b r > u_{\parallel} = \frac{\mathbf{u} \cdot \mathbf{v}}{|\mathbf{v}|} = \, \, \text{(signed length of the projection of } \mathbf{u} \text{ onto } \mathbf{v}). < / p > < / l i > < l i > < p > T h e r e l a t i o n s h i p b e t w e e n t h e t w o f o r m s < b r > </p></li><li><p>The relationship between the two forms<br> < / p >< / l i >< l i >< p > T h er e l a t i o n s hi p b e tw ee n t h e tw o f or m s < b r > \text{proj}{\mathbf{v}} \mathbf{u} = (u {\parallel}) \, \hat{\mathbf{v}} = \left( \frac{\mathbf{u} \cdot \mathbf{v}}{|\mathbf{v}|^2} \right) \, \mathbf{v}. < / p > < / l i > < l i > < p > G e o m e t r i c i n t e r p r e t a t i o n : T h e l e n g t h o f t h e p r o j e c t i o n i s ∣ u ∣ c o s θ , a n d i t s s i g n i s g i v e n b y t h e s i g n o f c o s θ v i a t h e d i r e c t i o n o f v ^ . < / p > < / l i > < / u l > < / l i > < l i > < p > W o r k e d e x a m p l e s o f p r o j e c t i o n a n d d e c o m p o s i t i o n ( i l l u s t r a t i v e ) < / p > < u l > < l i > < p > E x a m p l e A ( 3 D ) : L e t u = ( 6 , 3 , 2 ) a n d v = ( 1 , − 2 , − 2 ) . T h e n < b r > </p></li><li><p>Geometric interpretation: The length of the projection is |\mathbf{u}| cos \theta, and its sign is given by the sign of cos \theta via the direction of \hat{\mathbf{v}}.</p></li></ul></li><li><p>Worked examples of projection and decomposition (illustrative)</p><ul><li><p>Example A (3D): Let \mathbf{u} = (6, 3, 2) and \mathbf{v} = (1, -2, -2). Then<br> < / p >< / l i >< l i >< p > G eo m e t r i c in t er p r e t a t i o n : T h e l e n g t h o f t h e p r o j ec t i o ni s ∣ u ∣ cos θ , an d i t ss i g ni s g i v e nb y t h es i g n o f cos θ v ia t h e d i r ec t i o n o f v ^ . < / p >< / l i >< / u l >< / l i >< l i >< p > W or k e d e x am pl eso f p r o j ec t i o nan dd eco m p os i t i o n ( i l l u s t r a t i v e ) < / p >< u l >< l i >< p > E x am pl e A ( 3 D ) : L e t u = ( 6 , 3 , 2 ) an d v = ( 1 , − 2 , − 2 ) . T h e n < b r > \text{proj}_{\mathbf{v}} \mathbf{u} = \left( \frac{\mathbf{u} \cdot \mathbf{v}}{\mathbf{v} \cdot \mathbf{v}} \right) \mathbf{v} = \left( \frac{-4}{9} \right) (1, -2, -2) = \left( -\tfrac{4}{9}, \tfrac{8}{9}, \tfrac{8}{9} \right). < / p > < / l i > < l i > < p > S c a l a r c o m p o n e n t a l o n g v : < b r > </p></li><li><p>Scalar component along \mathbf{v}:<br> < / p >< / l i >< l i >< p > S c a l a r co m p o n e n t a l o n g v :< b r > u_{\parallel} = \frac{\mathbf{u} \cdot \mathbf{v}}{|\mathbf{v}|} = \frac{-4}{\sqrt{1+4+4}} = -\frac{4}{3}. < / p > < / l i > < l i > < p > I n 2 D , a s i m i l a r a p p r o a c h a p p l i e s ( E x a m p l e 6 i n t h e t r a n s c r i p t ) : f o r F = ( 5 , 2 ) a n d v = ( 1 , − 3 ) , < b r > </p></li><li><p>In 2D, a similar approach applies (Example 6 in the transcript): for F = (5, 2) and \mathbf{v} = (1, -3),<br> < / p >< / l i >< l i >< p > I n 2 D , a s imi l a r a pp r o a c ha ppl i es ( E x am pl e 6 in t h e t r an scr i pt ) : f or F = ( 5 , 2 ) an d v = ( 1 , − 3 ) , < b r > \text{proj}_{\mathbf{v}} \mathbf{F} = \left( \frac{F \cdot v}{v \cdot v} \right) v = \left( \frac{5(1) + 2(-3)}{1^2 + (-3)^2} ight) (1, -3) = \left( \frac{-1}{10} \right) (1, -3) = \left( -\tfrac{1}{10}, \tfrac{3}{10} \right). < / p > < / l i > < l i > < p > D e c o m p o s i t i o n i d e n t i t y : f o r a n y u a n d n o n z e r o v < b r > </p></li><li><p>Decomposition identity: for any \mathbf{u} and nonzero \mathbf{v}<br> < / p >< / l i >< l i >< p > D eco m p os i t i o ni d e n t i t y : f or an y u an d n o n z er o v < b r > \mathbf{u} = \text{proj}{\mathbf{v}} \mathbf{u} + (\mathbf{u} - \text{proj} {\mathbf{v}} \mathbf{u}), < b r > a n d t h e t w o s u m m a n d s a r e o r t h o g o n a l : < b r > <br>and the two summands are orthogonal:<br> < b r > an d t h e tw os u mman d s a r eor t h o g o na l :< b r > (\mathbf{u} - \text{proj}_{\mathbf{v}} \mathbf{u}) \cdot \mathbf{v} = 0. < / p > < / l i > < / u l > < / l i > < l i > < p > W o r k d o n e b y a c o n s t a n t f o r c e a l o n g a d i s p l a c e m e n t < / p > < u l > < l i > < p > I f a c o n s t a n t f o r c e F a c t s t h r o u g h a d i s p l a c e m e n t D , t h e w o r k i s < b r > </p></li></ul></li><li><p>Work done by a constant force along a displacement</p><ul><li><p>If a constant force \mathbf{F} acts through a displacement \mathbf{D}, the work is<br> < / p >< / l i >< / u l >< / l i >< l i >< p > W or k d o n e b y a co n s t an t f or ce a l o n g a d i s pl a ce m e n t < / p >< u l >< l i >< p > I f a co n s t an t f or ce F a c t s t h r o ug ha d i s pl a ce m e n t D , t h e w or k i s < b r > W = \mathbf{F} \cdot \mathbf{D}. < / p > < / l i > < l i > < p > I f t h e f o r c e m a k e s a n a n g l e θ w i t h t h e d i s p l a c e m e n t , t h e n < b r > </p></li><li><p>If the force makes an angle \theta with the displacement, then<br> < / p >< / l i >< l i >< p > I f t h e f or ce mak es anan g l e θ w i t h t h e d i s pl a ce m e n t , t h e n < b r > W = |\mathbf{F}| \, |\mathbf{D}| \, \cos \theta = \mathbf{F} \cdot \mathbf{D}. < / p > < / l i > < l i > < p > E x a m p l e : I f F = 40 N , ∣ D ∣ = 3 m , a n d θ = 60 e x t o , < b r > </p></li><li><p>Example: If F = 40 N, |D| = 3 m, and \theta = 60^ ext{o},<br> < / p >< / l i >< l i >< p > E x am pl e : I f F = 40 N , ∣ D ∣ = 3 m , an d θ = 6 0 e x t o , < b r > W = (40)(3) \cos 60^ ext{o} = 60 \, \text{J}. < / p > < / l i > < l i > < p > N o t e : C h a p t e r 16 e x t e n d s t h e s e i d e a s t o v a r i a b l e f o r c e s a l o n g g e n e r a l p a t h s . < / p > < / l i > < / u l > < / l i > < l i > < p > A d d i t i o n a l c o n t e x t a n d c o n n e c t i o n s < / p > < u l > < l i > < p > T h e d o t p r o d u c t i s a f o u n d a t i o n a l t o o l f o r g e o m e t r i c a n d p h y s i c a l c a l c u l a t i o n s i n b o t h s p a c e a n d t h e p l a n e . < / p > < / l i > < l i > < p > I t c o n n e c t s a l g e b r a i c o p e r a t i o n s w i t h g e o m e t r i c q u a n t i t i e s : a n g l e , p r o j e c t i o n , w o r k , a n d d e c o m p o s i t i o n s i n t o p a r a l l e l a n d p e r p e n d i c u l a r c o m p o n e n t s . < / p > < / l i > < / u l > < / l i > < l i > < p > S e l e c t e d p r o b l e m s f r o m C h a p t e r 12 ( 12.2 / 12.3 l e v e l , a s l i s t e d i n t h e t r a n s c r i p t ) < / p > < u l > < l i > < p > F i n d t h e v e c t o r f r o m t h e o r i g i n t o t h e p o i n t o f i n t e r s e c t i o n o f t h e m e d i a n s o f t r i a n g l e w i t h v e r t i c e s A ( 1 , − 1 , 2 ) , B ( 2 , 1 , 3 ) , C ( − 1 , 2 , − 1 ) . < / p > < / l i > < l i > < p > T h e m e d i a n s i n t e r s e c t a t t h e c e n t r o i d , w h i c h i s a t t h e a v e r a g e o f t h e v e r t e x c o o r d i n a t e s : < b r > </p></li><li><p>Note: Chapter 16 extends these ideas to variable forces along general paths.</p></li></ul></li><li><p>Additional context and connections</p><ul><li><p>The dot product is a foundational tool for geometric and physical calculations in both space and the plane.</p></li><li><p>It connects algebraic operations with geometric quantities: angle, projection, work, and decompositions into parallel and perpendicular components.</p></li></ul></li><li><p>Selected problems from Chapter 12 (12.2/12.3 level, as listed in the transcript)</p><ul><li><p>Find the vector from the origin to the point of intersection of the medians of triangle with vertices A(1, -1, 2), B(2, 1, 3), C(-1, 2, -1).</p></li><li><p>The medians intersect at the centroid, which is at the average of the vertex coordinates:<br> < / p >< / l i >< l i >< p > N o t e : C ha pt er 16 e x t e n d s t h ese i d e a s t o v a r iab l e f or ces a l o n g g e n er a l p a t h s . < / p >< / l i >< / u l >< / l i >< l i >< p > A dd i t i o na l co n t e x t an d co nn ec t i o n s < / p >< u l >< l i >< p > T h e d o tp r o d u c t i s a f o u n d a t i o na l t oo l f or g eo m e t r i c an d p h y s i c a l c a l c u l a t i o n s inb o t h s p a ce an d t h e pl an e . < / p >< / l i >< l i >< p > I t co nn ec t s a l g e b r ai co p er a t i o n s w i t h g eo m e t r i c q u an t i t i es : an g l e , p r o j ec t i o n , w or k , an dd eco m p os i t i o n s in t o p a r a l l e l an d p er p e n d i c u l a r co m p o n e n t s . < / p >< / l i >< / u l >< / l i >< l i >< p > S e l ec t e d p r o b l e m s f r o m C ha pt er 12 ( 12.2/12.3 l e v e l , a s l i s t e d in t h e t r an scr i pt ) < / p >< u l >< l i >< p > F in d t h e v ec t or f r o m t h eor i g in t o t h e p o in t o f in t er sec t i o n o f t h e m e d ian so f t r ian g l e w i t h v er t i ces A ( 1 , − 1 , 2 ) , B ( 2 , 1 , 3 ) , C ( − 1 , 2 , − 1 ) . < / p >< / l i >< l i >< p > T h e m e d ian s in t er sec t a tt h ece n t r o i d , w hi c hi s a tt h e a v er a g eo f t h e v er t e x coor d ina t es :< b r > ext{Centroid} = \left( \frac{1+2-1}{3}, \frac{-1+1+2}{3}, \frac{2+3-1}{3} \right) = \left( \frac{2}{3}, \frac{2}{3}, \frac{4}{3} \right). < / p > < / l i > < l i > < p > V e c t o r f r o m t h e o r i g i n t o t h e c e n t r o i d i s t h e s a m e a s t h e c e n t r o i d c o o r d i n a t e s : </p></li><li><p>Vector from the origin to the centroid is the same as the centroid coordinates: < / p >< / l i >< l i >< p > V ec t or f r o m t h eor i g in t o t h ece n t r o i d i s t h es am e a s t h ece n t r o i d coor d ina t es : \left( \tfrac{2}{3}, \tfrac{2}{3}, \tfrac{4}{3} \right). < / p > < / l i > < l i > < p > L e t A B C D b e a g e n e r a l , n o t n e c e s s a r i l y p l a n a r , q u a d r i l a t e r a l i n s p a c e . S h o w t h a t t h e t w o s e g m e n t s j o i n i n g t h e m i d p o i n t s o f o p p o s i t e s i d e s o f A B C D b i s e c t e a c h o t h e r . < / p > < / l i > < l i > < p > L e t A , B , C , D b e p o s i t i o n v e c t o r s . T h e m i d p o i n t s a r e : < / p > < u l > < l i > < p > M < e m > A B = ( A + B ) / 2 , M < / e m > C D = ( C + D ) / 2 f o r t h e s e g m e n t j o i n i n g A B a n d C D m i d p o i n t s . < / p > < / l i > < l i > < p > M < e m > B C = ( B + C ) / 2 , M < / e m > A D = ( A + D ) / 2 f o r t h e s e g m e n t j o i n i n g B C a n d A D m i d p o i n t s . < / p > < / l i > < / u l > < / l i > < l i > < p > T h e m i d p o i n t o f t h e s e g m e n t j o i n i n g M < e m > A B a n d M < / e m > C D i s < b r > </p></li><li><p>Let ABCD be a general, not necessarily planar, quadrilateral in space. Show that the two segments joining the midpoints of opposite sides of ABCD bisect each other.</p></li><li><p>Let A, B, C, D be position vectors. The midpoints are:</p><ul><li><p>M<em>AB = (A + B)/2, M</em>CD = (C + D)/2 for the segment joining AB and CD midpoints.</p></li><li><p>M<em>BC = (B + C)/2, M</em>AD = (A + D)/2 for the segment joining BC and AD midpoints.</p></li></ul></li><li><p>The midpoint of the segment joining M<em>AB and M</em>CD is<br> < / p >< / l i >< l i >< p > L e t A B C D b e a g e n er a l , n o t n ecess a r i l y pl ana r , q u a d r i l a t er a l in s p a ce . S h o w t ha tt h e tw ose g m e n t s j o inin g t h e mi d p o in t so f o pp os i t es i d eso f A B C D bi sec t e a c h o t h er . < / p >< / l i >< l i >< p > L e t A , B , C , D b e p os i t i o n v ec t or s . T h e mi d p o in t s a r e :< / p >< u l >< l i >< p > M < e m > A B = ( A + B ) /2 , M < / e m > C D = ( C + D ) /2 f or t h ese g m e n t j o inin g A B an d C D mi d p o in t s . < / p >< / l i >< l i >< p > M < e m > B C = ( B + C ) /2 , M < / e m > A D = ( A + D ) /2 f or t h ese g m e n t j o inin g B C an d A D mi d p o in t s . < / p >< / l i >< / u l >< / l i >< l i >< p > T h e mi d p o in t o f t h ese g m e n t j o inin g M < e m > A B an d M < / e m > C D i s < b r > rac{M{AB} + M {CD}}{2} = \frac{A + B + C + D}{4}. < / p > < / l i > < l i > < p > T h e m i d p o i n t o f t h e s e g m e n t j o i n i n g M < e m > B C a n d M < / e m > A D i s < b r > </p></li><li><p>The midpoint of the segment joining M<em>BC and M</em>AD is<br> < / p >< / l i >< l i >< p > T h e mi d p o in t o f t h ese g m e n t j o inin g M < e m > B C an d M < / e m > A D i s < b r > \frac{M{BC} + M {AD}}{2} = \frac{A + B + C + D}{4}. < / p > < / l i > < l i > < p > T h e r e f o r e t h e t w o s e g m e n t s s h a r e t h e s a m e m i d p o i n t a n d b i s e c t e a c h o t h e r . < / p > < / l i > < l i > < p > V e c t o r s d r a w n f r o m t h e c e n t e r o f a r e g u l a r n − s i d e d p o l y g o n i n t h e p l a n e t o t h e v e r t i c e s : s h o w t h e s u m o f t h e v e c t o r s i s z e r o . < / p > < / l i > < l i > < p > R e a s o n : r o t a t i o n a l s y m m e t r y . R o t a t i n g t h e p o l y g o n b y 360 ° / n p e r m u t e s t h e v e r t e x v e c t o r s ; t h e s u m m u s t b e i n v a r i a n t u n d e r t h i s r o t a t i o n , w h i c h f o r c e s t h e s u m t o b e t h e z e r o v e c t o r . < / p > < / l i > < l i > < p > I f A , B , C a r e v e r t i c e s o f a t r i a n g l e a n d a , b , c a r e r e s p e c t i v e l y t h e m i d p o i n t s o f t h e o p p o s i t e s i d e s , s h o w t h a t A a + B b + C c = 0. < / p > < / l i > < l i > < p > L e t a b e t h e m i d p o i n t o f B C , b o f C A , c o f A B . T h e n a = ( B + C ) / 2 , e t c . C o m p u t e : < b r > </p></li><li><p>Therefore the two segments share the same midpoint and bisect each other.</p></li><li><p>Vectors drawn from the center of a regular n-sided polygon in the plane to the vertices: show the sum of the vectors is zero.</p></li><li><p>Reason: rotational symmetry. Rotating the polygon by 360°/n permutes the vertex vectors; the sum must be invariant under this rotation, which forces the sum to be the zero vector.</p></li><li><p>If A, B, C are vertices of a triangle and a, b, c are respectively the midpoints of the opposite sides, show that \mathbf{A}\mathbf{a} + \mathbf{B}\mathbf{b} + \mathbf{C}\mathbf{c} = 0.</p></li><li><p>Let a be the midpoint of BC, b of CA, c of AB. Then a = (B + C)/2, etc. Compute:<br> < / p >< / l i >< l i >< p > T h er e f or e t h e tw ose g m e n t ss ha r e t h es am e mi d p o in t an d bi sec t e a c h o t h er . < / p >< / l i >< l i >< p > V ec t or s d r a w n f r o m t h ece n t er o f a r e g u l a r n − s i d e d p o l y g o nin t h e pl an e t o t h e v er t i ces : s h o w t h es u m o f t h e v ec t or s i sz er o . < / p >< / l i >< l i >< p > R e a so n : r o t a t i o na l sy mm e t r y . R o t a t in g t h e p o l y g o nb y 360°/ n p er m u t es t h e v er t e xv ec t or s ; t h es u mm u s t b e in v a r ian t u n d er t hi sr o t a t i o n , w hi c h f or ces t h es u m t o b e t h ez er o v ec t or . < / p >< / l i >< l i >< p > I f A , B , C a r e v er t i ceso f a t r ian g l e an d a , b , c a r er es p ec t i v e l y t h e mi d p o in t so f t h eo pp os i t es i d es , s h o w t ha t Aa + Bb + Cc = 0. < / p >< / l i >< l i >< p > L e t ab e t h e mi d p o in t o f B C , b o f C A , co f A B . T h e na = ( B + C ) /2 , e t c . C o m p u t e :< b r > \mathbf{A} \mathbf{a} + \mathbf{B} \mathbf{b} + \mathbf{C} \mathbf{c} = (A - A) + (B - B) + (C - C) = 0, < / p > < / l i > < l i > < p > o r m o r e e x p l i c i t l y b y w r i t i n g a − A = ( B + C ) / 2 − A , e t c . , a n d s u m m i n g . < / p > < / l i > < l i > < p > U n i t v e c t o r s i n t h e p l a n e : s h o w t h a t a u n i t v e c t o r c a n b e e x p r e s s e d a s </p></li><li><p>or more explicitly by writing a - A = (B + C)/2 - A, etc., and summing.</p></li><li><p>Unit vectors in the plane: show that a unit vector can be expressed as < / p >< / l i >< l i >< p > or m or ee x pl i c i tl y b y w r i t in g a − A = ( B + C ) /2 − A , e t c . , an d s u mmin g . < / p >< / l i >< l i >< p > U ni t v ec t or s in t h e pl an e : s h o w t ha t a u ni t v ec t or c anb ee x p r esse d a s \mathbf{u} = (\cos \theta) \mathbf{i} + (\sin \theta) \mathbf{j}, o b t a i n e d b y r o t a t i n g t h e s t a n d a r d b a s i s v e c t o r i t h r o u g h a n a n g l e θ i n t h e c o u n t e r c l o c k w i s e d i r e c t i o n . < / p > < / l i > < l i > < p > T h i s p a r a m e t e r i z a t i o n c o v e r s e v e r y d i r e c t i o n i n t h e p l a n e a s θ r a n g e s o v e r [ 0 , 2 π ) . T h e l e n g t h i s 1 b e c a u s e cos 2 θ + sin 2 θ = 1. < / p > < / l i > < / u l > < / l i > < l i > < p > P r a c t i c a l t a k e a w a y < / p > < u l > < l i > < p > T h e d o t p r o d u c t i s t h e p r i m a r y t o o l f o r c o n v e r t i n g a n g l e a n d p r o j e c t i o n q u e s t i o n s i n t o a l g e b r a i c c o m p u t a t i o n s v i a c o m p o n e n t s u m s . < / p > < / l i > < l i > < p > I t p r o v i d e s a d i r e c t r o u t e t o w o r k c a l c u l a t i o n s v i a F ⋅ D i n s t e a d o f r e s o l v i n g F i n t o c o m p o n e n t s a l o n g a p a t h . < / p > < / l i > < / u l > < / l i > < l i > < p > S u m m a r y o f k e y f o r m u l a s t o m e m o r i z e < / p > < u l > < l i > < p > D o t p r o d u c t ( 3 D ) : obtained by rotating the standard basis vector \mathbf{i} through an angle \theta in the counterclockwise direction.</p></li><li><p>This parameterization covers every direction in the plane as \theta ranges over [0, 2π). The length is 1 because \cos^2 \theta + \sin^2 \theta = 1.</p></li></ul></li><li><p>Practical takeaway</p><ul><li><p>The dot product is the primary tool for converting angle and projection questions into algebraic computations via component sums.</p></li><li><p>It provides a direct route to work calculations via F \cdot D instead of resolving F into components along a path.</p></li></ul></li><li><p>Summary of key formulas to memorize</p><ul><li><p>Dot product (3D): o b t ain e d b y r o t a t in g t h es t an d a r d ba s i s v ec t or i t h r o ug hanan g l e θ in t h eco u n t er c l oc k w i se d i r ec t i o n . < / p >< / l i >< l i >< p > T hi s p a r am e t er i z a t i o n co v er se v er y d i r ec t i o nin t h e pl an e a s θ r an g eso v er [ 0 , 2 π ) . T h e l e n g t hi s 1 b ec a u se cos 2 θ + sin 2 θ = 1. < / p >< / l i >< / u l >< / l i >< l i >< p > P r a c t i c a l t ak e a w a y < / p >< u l >< l i >< p > T h e d o tp r o d u c t i s t h e p r ima r y t oo l f or co n v er t in g an g l e an d p r o j ec t i o n q u es t i o n s in t o a l g e b r ai cco m p u t a t i o n s v ia co m p o n e n t s u m s . < / p >< / l i >< l i >< p > I tp r o v i d es a d i r ec t r o u t e t o w or k c a l c u l a t i o n s v ia F ⋅ D in s t e a d o f r eso l v in g F in t oco m p o n e n t s a l o n g a p a t h . < / p >< / l i >< / u l >< / l i >< l i >< p > S u mma r y o f k ey f or m u l a s t o m e m or i z e < / p >< u l >< l i >< p > D o tp r o d u c t ( 3 D ) : \mathbf{u} \cdot \mathbf{v} = u1 v 1 + u2 v 2 + u3 v 3. < / p > < / l i > < l i > < p > M a g n i t u d e : </p></li><li><p>Magnitude: < / p >< / l i >< l i >< p > M a g ni t u d e : |\mathbf{u}| = \sqrt{u1^2 + u 2^2 + u_3^2}. < / p > < / l i > < l i > < p > A n g l e b e t w e e n v e c t o r s : </p></li><li><p>Angle between vectors: < / p >< / l i >< l i >< p > A n g l e b e tw ee n v ec t or s : \cos \theta = \frac{\mathbf{u} \cdot \mathbf{v}}{|\mathbf{u}| \, |\mathbf{v}|}. < / p > < / l i > < l i > < p > V e c t o r p r o j e c t i o n o n t o v : </p></li><li><p>Vector projection onto v: < / p >< / l i >< l i >< p > V ec t or p r o j ec t i o n o n t o v : \text{proj}_{\mathbf{v}} \mathbf{u} = \left( \frac{\mathbf{u} \cdot \mathbf{v}}{\mathbf{v} \cdot \mathbf{v}} \right) \mathbf{v}. < / p > < / l i > < l i > < p > S c a l a r c o m p o n e n t a l o n g v : </p></li><li><p>Scalar component along v: < / p >< / l i >< l i >< p > S c a l a r co m p o n e n t a l o n g v : u_{\parallel} = \frac{\mathbf{u} \cdot \mathbf{v}}{|\mathbf{v}|} = \mathbf{u} \\cdot \hat{\mathbf{v}}. < / p > < / l i > < l i > < p > D e c o m p o s i t i o n : </p></li><li><p>Decomposition: < / p >< / l i >< l i >< p > D eco m p os i t i o n : \mathbf{u} = \text{proj}{\mathbf{v}} \mathbf{u} + (\mathbf{u} - \text{proj} {\mathbf{v}} \mathbf{u}), \quad (\mathbf{u} - \text{proj}_{\mathbf{v}} \mathbf{u}) \cdot \mathbf{v} = 0. < / p > < / l i > < l i > < p > W o r k d o n e b y c o n s t a n t f o r c e : </p></li><li><p>Work done by constant force: < / p >< / l i >< l i >< p > W or k d o n e b y co n s t an t f or ce : W = \mathbf{F} \cdot \mathbf{D} = |\mathbf{F}| \, |\mathbf{D}| \, \cos \theta. $$