← 2022 Paper 1
UPSC 2022 Maths Optional Paper 1 Q4c — Step-by-Step Solution 15 marks · Section A
Cone · Analytic Geometry · asked 14× in 13 yrs · Read the full method →
Question
If the plane u x + v y + w z = 0 ux+vy+wz=0 ux + v y + w z = 0 cuts the cone a x 2 + b y 2 + c z 2 = 0 ax^2+by^2+cz^2=0 a x 2 + b y 2 + c z 2 = 0 in perpendicular generators, then prove that ( b + c ) u 2 + ( c + a ) v 2 + ( a + b ) w 2 = 0 (b+c)u^2+(c+a)v^2+(a+b)w^2=0 ( b + c ) u 2 + ( c + a ) v 2 + ( a + b ) w 2 = 0 .
Technique
Parametrise the line of intersection of plane and cone; treat as a quadratic in slope ratio; use Vieta + perpendicularity condition l 1 l 2 + m 1 m 2 + n 1 n 2 = 0 l_1 l_2+m_1 m_2+n_1 n_2=0 l 1 l 2 + m 1 m 2 + n 1 n 2 = 0 .
Solution
Setup. Both surfaces pass through the origin. The plane u x + v y + w z = 0 ux+vy+wz=0 ux + v y + w z = 0 also passes through the origin (no constant term). The intersection of the plane with the cone consists of two lines through the origin — these are the “generators”.
Let the two generators have direction vectors ℓ ⃗ 1 = ( l 1 , m 1 , n 1 ) \vec\ell_1=(l_1,m_1,n_1) ℓ 1 = ( l 1 , m 1 , n 1 ) and ℓ ⃗ 2 = ( l 2 , m 2 , n 2 ) \vec\ell_2=(l_2,m_2,n_2) ℓ 2 = ( l 2 , m 2 , n 2 ) . Each direction must:
Lie on the cone: a l 2 + b m 2 + c n 2 = 0 a l^2+b m^2+c n^2=0 a l 2 + b m 2 + c n 2 = 0 .
Lie on the plane: u l + v m + w n = 0 u l+v m+w n=0 u l + v m + w n = 0 .
Step 1 — Parametrise direction on the plane
From the plane equation: w n = − ( u l + v m ) w n=-(u l+v m) w n = − ( u l + v m ) , so n = − ( u l + v m ) / w n=-(ul+vm)/w n = − ( u l + v m ) / w (assuming w ≠ 0 w\ne 0 w = 0 ).
Substitute into the cone equation:
a l 2 + b m 2 + c ⋅ ( u l + v m ) 2 w 2 = 0. a l^2+b m^2+c\cdot\dfrac{(ul+vm)^2}{w^2}=0. a l 2 + b m 2 + c ⋅ w 2 ( u l + v m ) 2 = 0.
Multiply by w 2 w^2 w 2 :
a w 2 l 2 + b w 2 m 2 + c ( u l + v m ) 2 = 0 , a w^2 l^2+b w^2 m^2+c(ul+vm)^2=0, a w 2 l 2 + b w 2 m 2 + c ( u l + v m ) 2 = 0 ,
a w 2 l 2 + b w 2 m 2 + c ( u 2 l 2 + 2 u v l m + v 2 m 2 ) = 0 , a w^2 l^2+b w^2 m^2+c(u^2 l^2+2uvlm+v^2 m^2)=0, a w 2 l 2 + b w 2 m 2 + c ( u 2 l 2 + 2 uv l m + v 2 m 2 ) = 0 ,
( a w 2 + c u 2 ) l 2 + 2 c u v l m + ( b w 2 + c v 2 ) m 2 = 0. (a w^2+c u^2)l^2+2cuvlm+(b w^2+c v^2)m^2=0. ( a w 2 + c u 2 ) l 2 + 2 c uv l m + ( b w 2 + c v 2 ) m 2 = 0.
Step 2 — Treat as quadratic in l / m l/m l / m
Set t = l / m t=l/m t = l / m . The quadratic is
( a w 2 + c u 2 ) t 2 + 2 c u v t + ( b w 2 + c v 2 ) = 0. (a w^2+c u^2)t^2+2cuv\,t+(b w^2+c v^2)=0. ( a w 2 + c u 2 ) t 2 + 2 c uv t + ( b w 2 + c v 2 ) = 0.
The two roots t 1 = l 1 / m 1 t_1=l_1/m_1 t 1 = l 1 / m 1 and t 2 = l 2 / m 2 t_2=l_2/m_2 t 2 = l 2 / m 2 correspond to the two generators.
By Vieta:
t 1 + t 2 = − 2 c u v a w 2 + c u 2 t_1+t_2=-\dfrac{2cuv}{aw^2+cu^2} t 1 + t 2 = − a w 2 + c u 2 2 c uv .
t 1 t 2 = b w 2 + c v 2 a w 2 + c u 2 t_1 t_2=\dfrac{bw^2+cv^2}{aw^2+cu^2} t 1 t 2 = a w 2 + c u 2 b w 2 + c v 2 .
Step 3 — Perpendicularity condition
ℓ ⃗ 1 ⊥ ℓ ⃗ 2 ⇔ l 1 l 2 + m 1 m 2 + n 1 n 2 = 0 \vec\ell_1\perp\vec\ell_2\Leftrightarrow l_1 l_2+m_1 m_2+n_1 n_2=0 ℓ 1 ⊥ ℓ 2 ⇔ l 1 l 2 + m 1 m 2 + n 1 n 2 = 0 .
Dividing by m 1 m 2 m_1 m_2 m 1 m 2 :
l 1 l 2 m 1 m 2 + 1 + n 1 n 2 m 1 m 2 = 0 , \dfrac{l_1 l_2}{m_1 m_2}+1+\dfrac{n_1 n_2}{m_1 m_2}=0, m 1 m 2 l 1 l 2 + 1 + m 1 m 2 n 1 n 2 = 0 ,
i.e. t 1 t 2 + 1 + n 1 n 2 m 1 m 2 = 0 t_1 t_2+1+\dfrac{n_1 n_2}{m_1 m_2}=0 t 1 t 2 + 1 + m 1 m 2 n 1 n 2 = 0 .
Step 4 — Compute n 1 n 2 / ( m 1 m 2 ) n_1 n_2/(m_1 m_2) n 1 n 2 / ( m 1 m 2 )
From plane: n = − ( u l + v m ) / w = − u t + v w ⋅ m / m n=-(ul+vm)/w=-\dfrac{u t+v}{w}\cdot m\;/m n = − ( u l + v m ) / w = − w u t + v ⋅ m / m — let me redo.
n i = − ( u l i + v m i ) / w n_i=-(u l_i+v m_i)/w n i = − ( u l i + v m i ) / w , so n i / m i = − ( u t i + v ) / w n_i/m_i=-(u t_i+v)/w n i / m i = − ( u t i + v ) / w .
Hence n 1 n 2 m 1 m 2 = ( u t 1 + v ) ( u t 2 + v ) w 2 = u 2 t 1 t 2 + u v ( t 1 + t 2 ) + v 2 w 2 \dfrac{n_1 n_2}{m_1 m_2}=\dfrac{(u t_1+v)(u t_2+v)}{w^2}=\dfrac{u^2 t_1 t_2+uv(t_1+t_2)+v^2}{w^2} m 1 m 2 n 1 n 2 = w 2 ( u t 1 + v ) ( u t 2 + v ) = w 2 u 2 t 1 t 2 + uv ( t 1 + t 2 ) + v 2 .
Substitute Vieta:
u 2 ⋅ b w 2 + c v 2 a w 2 + c u 2 + u v ⋅ − 2 c u v a w 2 + c u 2 + v 2 u^2\cdot\dfrac{bw^2+cv^2}{aw^2+cu^2}+uv\cdot\dfrac{-2cuv}{aw^2+cu^2}+v^2 u 2 ⋅ a w 2 + c u 2 b w 2 + c v 2 + uv ⋅ a w 2 + c u 2 − 2 c uv + v 2
= u 2 ( b w 2 + c v 2 ) − 2 c u 2 v 2 a w 2 + c u 2 + v 2 =\dfrac{u^2(bw^2+cv^2)-2cu^2 v^2}{aw^2+cu^2}+v^2 = a w 2 + c u 2 u 2 ( b w 2 + c v 2 ) − 2 c u 2 v 2 + v 2
= u 2 b w 2 + u 2 c v 2 − 2 c u 2 v 2 a w 2 + c u 2 + v 2 =\dfrac{u^2 b w^2+u^2 c v^2-2cu^2 v^2}{aw^2+cu^2}+v^2 = a w 2 + c u 2 u 2 b w 2 + u 2 c v 2 − 2 c u 2 v 2 + v 2
= u 2 b w 2 − c u 2 v 2 a w 2 + c u 2 + v 2 =\dfrac{u^2 b w^2-cu^2 v^2}{aw^2+cu^2}+v^2 = a w 2 + c u 2 u 2 b w 2 − c u 2 v 2 + v 2
= u 2 b w 2 − c u 2 v 2 + v 2 ( a w 2 + c u 2 ) a w 2 + c u 2 =\dfrac{u^2 b w^2-cu^2 v^2+v^2(aw^2+cu^2)}{aw^2+cu^2} = a w 2 + c u 2 u 2 b w 2 − c u 2 v 2 + v 2 ( a w 2 + c u 2 )
= u 2 b w 2 − c u 2 v 2 + a v 2 w 2 + c u 2 v 2 a w 2 + c u 2 =\dfrac{u^2 b w^2-cu^2 v^2+a v^2 w^2+cu^2 v^2}{aw^2+cu^2} = a w 2 + c u 2 u 2 b w 2 − c u 2 v 2 + a v 2 w 2 + c u 2 v 2
= u 2 b w 2 + a v 2 w 2 a w 2 + c u 2 = w 2 ( a u 2 . . . a w 2 + c u 2 . =\dfrac{u^2 b w^2+a v^2 w^2}{aw^2+cu^2}=\dfrac{w^2(au^2... }{aw^2+cu^2}. = a w 2 + c u 2 u 2 b w 2 + a v 2 w 2 = a w 2 + c u 2 w 2 ( a u 2 ... .
Wait — let me recompute: u 2 b w 2 + a v 2 w 2 = w 2 ( b u 2 + a v 2 ) u^2 b w^2+a v^2 w^2=w^2(bu^2+av^2) u 2 b w 2 + a v 2 w 2 = w 2 ( b u 2 + a v 2 ) .
So n 1 n 2 m 1 m 2 = w 2 ( b u 2 + a v 2 ) w 2 ( a w 2 + c u 2 ) = b u 2 + a v 2 a w 2 + c u 2 \dfrac{n_1 n_2}{m_1 m_2}=\dfrac{w^2(bu^2+av^2)}{w^2(aw^2+cu^2)}=\dfrac{bu^2+av^2}{aw^2+cu^2} m 1 m 2 n 1 n 2 = w 2 ( a w 2 + c u 2 ) w 2 ( b u 2 + a v 2 ) = a w 2 + c u 2 b u 2 + a v 2 .
(Dividing both numerator and denominator by w 2 w^2 w 2 .)
Step 5 — Assemble perpendicularity
t 1 t 2 + 1 + n 1 n 2 m 1 m 2 = 0 , t_1 t_2+1+\dfrac{n_1 n_2}{m_1 m_2}=0, t 1 t 2 + 1 + m 1 m 2 n 1 n 2 = 0 ,
i.e.
b w 2 + c v 2 a w 2 + c u 2 + 1 + b u 2 + a v 2 a w 2 + c u 2 = 0. \dfrac{bw^2+cv^2}{aw^2+cu^2}+1+\dfrac{bu^2+av^2}{aw^2+cu^2}=0. a w 2 + c u 2 b w 2 + c v 2 + 1 + a w 2 + c u 2 b u 2 + a v 2 = 0.
Multiply by ( a w 2 + c u 2 ) (aw^2+cu^2) ( a w 2 + c u 2 ) :
( b w 2 + c v 2 ) + ( a w 2 + c u 2 ) + ( b u 2 + a v 2 ) = 0. (bw^2+cv^2)+(aw^2+cu^2)+(bu^2+av^2)=0. ( b w 2 + c v 2 ) + ( a w 2 + c u 2 ) + ( b u 2 + a v 2 ) = 0.
Expand:
b w 2 + c v 2 + a w 2 + c u 2 + b u 2 + a v 2 = 0. bw^2+cv^2+aw^2+cu^2+bu^2+av^2=0. b w 2 + c v 2 + a w 2 + c u 2 + b u 2 + a v 2 = 0.
Group by u 2 , v 2 , w 2 u^2,v^2,w^2 u 2 , v 2 , w 2 :
Coefficient of u 2 u^2 u 2 : c + b = b + c c+b=b+c c + b = b + c .
Coefficient of v 2 v^2 v 2 : c + a = c + a c+a=c+a c + a = c + a .
Coefficient of w 2 w^2 w 2 : b + a = a + b b+a=a+b b + a = a + b .
( b + c ) u 2 + ( c + a ) v 2 + ( a + b ) w 2 = 0. ■ (b+c)u^2+(c+a)v^2+(a+b)w^2=0.\qquad\blacksquare ( b + c ) u 2 + ( c + a ) v 2 + ( a + b ) w 2 = 0. ■
Answer
( b + c ) u 2 + ( c + a ) v 2 + ( a + b ) w 2 = 0. \boxed{\;(b+c)u^2+(c+a)v^2+(a+b)w^2=0.\;} ( b + c ) u 2 + ( c + a ) v 2 + ( a + b ) w 2 = 0.