Advanced Vector Calculus and Matrix Algebra Problems
Cayley-Hamilton Theorem: Verification and Inverse
Problem 1: Verify Cayley-Hamilton theorem for A and find A-1
Given matrix: A = [[2, 1, 1], [0, 1, 0], [1, 1, 2]]
Step 1: Find the Characteristic Equation |A – λI| = 0
A – λI = [[2-λ, 1, 1], [0, 1-λ, 0], [1, 1, 2-λ]]
Expand along the 2nd row (which has two zeros):
|A – λI| = (1-λ) × |[2-λ, 1], [1, 2-λ]|
= (1-λ) × [(2-λ)(2-λ) – 1×1]
= (1-λ) × [(2-λ)2 – 1]
= (1-λ) × [4 – 4λ + λ2 – 1]
= (1-λ)(λ2 – 4λ + 3)
= (1-λ)(λ-1)(λ-3)
= -(λ-1)2(λ-3) = 0
Characteristic Equation: λ3 – 5λ2 + 7λ – 3 = 0
Step 2: Verify Cayley-Hamilton (A satisfies its own characteristic equation)
We must show: A3 – 5A2 + 7A – 3I = O (Zero matrix)
Calculate A2:
A2 = A × A = [[5, 4, 4], [0, 1, 0], [4, 4, 5]]
Calculate A3:
A3 = A2 × A = [[14, 13, 14], [0, 1, 0], [13, 13, 14]]
Now compute A3 – 5A2 + 7A – 3I:
= [[14, 13, 14],[0, 1, 0],[13, 13, 14]] – 5[[5, 4, 4],[0, 1, 0],[4, 4, 5]] + 7[[2, 1, 1],[0, 1, 0],[1, 1, 2]] – 3[[1, 0, 0],[0, 1, 0],[0, 0, 1]]
= [[0, 0, 0], [0, 0, 0], [0, 0, 0]] = O. ✓ Verified!
Step 3: Find A-1 using Cayley-Hamilton
From A3 – 5A2 + 7A – 3I = O
Multiply both sides by A-1:
A2 – 5A + 7I – 3A-1 = O
3A-1 = A2 – 5A + 7I
A-1 = (1/3)[A2 – 5A + 7I]
Calculate A2 – 5A + 7I:
= [[5, 4, 4],[0, 1, 0],[4, 4, 5]] – 5[[2, 1, 1],[0, 1, 0],[1, 1, 2]] + 7[[1, 0, 0],[0, 1, 0],[0, 0, 1]]
= [[5-10+7, 4-5+0, 4-5+0], [0, 1-5+7, 0], [4-5+0, 4-5+0, 5-10+7]]
= [[2, -1, -1], [0, 3, 0], [-1, -1, 2]]
A-1 = (1/3) × [[2, -1, -1], [0, 3, 0], [-1, -1, 2]]
Finding Eigenvalues and Eigenvectors for Matrix A
Problem 2: Find eigenvalues and eigenvectors of A
Given matrix: A = [[2, 1, 1], [2, 3, 2], [3, 3, 4]]
Step 1: Find Eigenvalues from |A – λI| = 0
|A – λI| = |[2-λ, 1, 1], [2, 3-λ, 2], [3, 3, 4-λ]| = 0
Expand (using R1):
= (2-λ)[(3-λ)(4-λ) – 6] – 1[2(4-λ) – 6] + 1[6 – 3(3-λ)]
= (2-λ)[λ2 – 7λ + 6] – [2 – 2λ] + [3λ – 3]
= (λ-1)[(2-λ)(λ-6) + 5]
= -(λ-1)(λ2 – 8λ + 7)
= -(λ-1)2(λ-7) = 0
Eigenvalues: λ1 = 1 (repeated), λ2 = 7
Step 2: Find Eigenvectors for λ = 1
Solve (A – 1·I)X = 0
[A – I] = [[1, 1, 1], [2, 2, 2], [3, 3, 3]]
Row reduce: All rows are proportional, leading to the equation x + y + z = 0.
- Let y = 1, z = 0 → x = -1: X1 = [-1, 1, 0]T
- Let y = 0, z = 1 → x = -1: X2 = [-1, 0, 1]T
Step 3: Find Eigenvector for λ = 7
Solve (A – 7I)X = 0
[A – 7I] = [[-5, 1, 1], [2, -4, 2], [3, 3, -3]]
Row reduce and solve: X3 = [1, 2, 3]T
Answer: For λ=1, X1=[-1, 1, 0]T, X2=[-1, 0, 1]T | For λ=7, X3=[1, 2, 3]T
Leibnitz Theorem Proof for Higher Order Derivatives
Problem 3: Prove the relation for y = etan⁻¹x
If y = etan⁻¹x, prove that (1+x2)yn+2 + [(2n+2)x – 1]yn+1 + n(n+1)yn = 0
Step 1: Find y1 (First Derivative)
y = etan⁻¹x
y1 = etan⁻¹x × 1/(1+x2) = y/(1+x2)
(1 + x2)y1 = y … (1)
Step 2: Find y2 (Differentiate equation 1)
Differentiating (1) using the product rule:
(1+x2)y2 + 2xy1 = y1
(1+x2)y2 + (2x-1)y1 = 0 … (2)
Step 3: Apply Leibnitz Theorem to equation (2)
Leibnitz Formula for the nth derivative of a product (uv)n: (uv)n = Σ nCr un-r vr
Differentiate equation (2) n times using Leibnitz:
For (1+x2)y2:
[(1+x2)y2]n = (1+x2)yn+2 + nC1(2x)yn+1 + nC2(2)yn
= (1+x2)yn+2 + 2nx yn+1 + n(n-1)yn
For (2x-1)y1:
[(2x-1)y1]n = (2x-1)yn+1 + nC1(2)yn
= (2x-1)yn+1 + 2n yn
Step 4: Combine and Simplify
Summing the results:
(1+x2)yn+2 + 2nx yn+1 + n(n-1)yn + (2x-1)yn+1 + 2n yn = 0
Group terms by derivative order:
(1+x2)yn+2 + (2nx + 2x – 1)yn+1 + [n(n-1) + 2n]yn = 0
(1+x2)yn+2 + [(2n+2)x – 1]yn+1 + [n2 – n + 2n]yn = 0
(1+x2)yn+2 + [(2n+2)x – 1]yn+1 + n(n+1)yn = 0
✓ Hence Proved!
Taylor Series Expansion of f(x,y) = xy about (1,1)
Problem 4: Expand f(x,y) and approximate (1.1)1.02
Function: f(x,y) = xy. Expansion point: (a,b) = (1, 1). We expand up to second degree terms.
Step 1: Taylor’s Formula for Two Variables
f(x,y) = f(a,b) + [(x-a)fx + (y-b)fy] + (1/2!)[(x-a)2fxx + 2(x-a)(y-b)fxy + (y-b)2fyy] + …
We expand in powers of (x-1) and (y-1).
Step 2: Calculate Required Partial Derivatives at (1,1)
- f(x,y) = xy → f(1,1) = 11 = 1
- fx = y xy-1 → fx(1,1) = 1 × 10 = 1
- fy = xy ln(x) → fy(1,1) = 11 × ln(1) = 0
- fxx = y(y-1)xy-2 → fxx(1,1) = 1 × 0 × 1 = 0
- fyy = xy (ln x)2 → fyy(1,1) = 1 × 0 = 0
- fxy = xy-1 + y xy-1 ln(x) → fxy(1,1) = 1 + 0 = 1
Step 3: Substitute into Taylor’s Formula
xy = 1 + [(x-1)×1 + (y-1)×0] + (1/2)[0 + 2(x-1)(y-1)×1 + 0] + …
xy = 1 + (x-1) + (x-1)(y-1) + …
Approximation: xy ≈ 1 + (x-1) + (x-1)(y-1)
Step 4: Find (1.1)1.02
Here x = 1.1, y = 1.02. Thus, (x-1) = 0.1 and (y-1) = 0.02.
(1.1)1.02 ≈ 1 + 0.1 + (0.1)(0.02)
= 1 + 0.1 + 0.002
= 1.102
Answer: (1.1)1.02 ≈ 1.102
Euler’s Theorem Application: Proving a Partial Derivative Relation
Problem 5: Prove x(∂u/∂x) + y(∂u/∂y) = 2tan(u) for u = sin⁻¹[(x³+y³)/(x+y)]
Step 1: Recognize the Homogeneous Function
Let v = sin(u) = (x³+y³)/(x+y)
Check the degree of homogeneity for v:
v(tx, ty) = (t³x³ + t³y³)/(tx + ty) = t³(x³+y³)/t(x+y) = t²v
v is homogeneous of degree n = 2.
Step 2: Apply Euler’s Theorem
Euler’s Theorem states: If v is homogeneous of degree n, then x(∂v/∂x) + y(∂v/∂y) = nv
For v = sin(u) and n = 2:
x(∂v/∂x) + y(∂v/∂y) = 2v = 2sin(u) … (1)
Step 3: Express in terms of u
Since v = sin(u), we use the chain rule:
- ∂v/∂x = cos(u) × ∂u/∂x
- ∂v/∂y = cos(u) × ∂u/∂y
Substitute these into equation (1):
x [cos(u) × ∂u/∂x] + y [cos(u) × ∂u/∂y] = 2sin(u)
Factor out cos(u):
cos(u) [x(∂u/∂x) + y(∂u/∂y)] = 2sin(u)
Divide by cos(u):
x(∂u/∂x) + y(∂u/∂y) = 2sin(u)/cos(u)
x(∂u/∂x) + y(∂u/∂y) = 2tan(u)
✓ Proved!
Calculating the Jacobian ∂(x,y)/∂(u,v)
Problem 6: Find the Jacobian for x = evsec(u) and y = evtan(u)
Step 1: Jacobian Definition
The Jacobian J is defined as the determinant of the matrix of partial derivatives:
J = ∂(x,y)/∂(u,v) = | ∂x/∂u ∂x/∂v | | ∂y/∂u ∂y/∂v |
Step 2: Calculate Partial Derivatives
Given x = evsec(u):
- ∂x/∂u = ev sec(u)tan(u)
- ∂x/∂v = sec(u) ev
Given y = evtan(u):
- ∂y/∂u = ev sec²(u)
- ∂y/∂v = tan(u) ev
Step 3: Calculate the Determinant
J = (evsec(u)tan(u)) × (evtan(u)) – (evsec(u)) × (evsec²(u))
= e2vsec(u)tan²(u) – e2vsec³(u)
Factor out e2vsec(u):
= e2vsec(u) [tan²(u) – sec²(u)]
Using the identity sec²(u) – tan²(u) = 1:
= e2vsec(u) [- (sec²(u) – tan²(u))]
= e2vsec(u) [-1]
∂(x,y)/∂(u,v) = -e2vsec(u)
Lagrange Multipliers: Minimizing Surface Area of a Box
Problem 7: Find dimensions for a rectangular box (open top) with capacity 32 ft³ for least material.
Step 1: Set up the Problem
Let length = x, width = y, height = z.
Constraint (Volume G): G(x, y, z) = xyz – 32 = 0
Objective (Surface Area S, open box): S(x, y, z) = xy + 2xz + 2yz
Step 2: Form the Lagrangian Function
F(x, y, z, λ) = S + λG = xy + 2xz + 2yz + λ(xyz – 32)
Step 3: Find Partial Derivatives and Set to Zero
- ∂F/∂x = y + 2z + λyz = 0 … (1)
- ∂F/∂y = x + 2z + λxz = 0 … (2)
- ∂F/∂z = 2x + 2y + λxy = 0 … (3)
- ∂F/∂λ = xyz – 32 = 0 … (4)
Step 4: Solve the System
From (1): λ = -(y + 2z)/(yz) = -1/z – 2/y
From (2): λ = -(x + 2z)/(xz) = -1/z – 2/x
Equating the expressions for λ:
-1/z – 2/y = -1/z – 2/x
Therefore: 2/y = 2/x → x = y
Substitute x = y into (3):
λ = -(2x + 2x)/(x²) = -4/x
Now equate this λ with the expression derived from (1) (using y=x):
-4/x = -1/z – 2/x → -2/x = -1/z → z = x/2
Step 5: Use Constraint to Find Values
Substitute x=y and z=x/2 into the volume constraint (4):
x × x × (x/2) = 32
x³/2 = 32
x³ = 64
x = 4
Since x=y=4 and z=x/2=2:
Answer: Length = 4 ft, Width = 4 ft, Height = 2 ft
Changing the Order of Integration and Evaluation
Problem 8: Change the order of integration and evaluate: ∫₀¹ ∫ₓ²²⁻ₓ xy dy dx
Step 1: Identify the Region of Integration
The original limits define the region R:
- x: 0 ≤ x ≤ 1
- y: x² ≤ y ≤ 2-x
The boundaries are the parabola y = x² and the line y = 2-x. The intersection is at x = 1, y = 1.
Step 2: Sketch and Divide Region for dx dy order
We express x as a function of y:
- Lower boundary: y = x² → x = √y
- Upper boundary: y = 2-x → x = 2-y
The region must be split at y = 1:
- Region R₁ (0 ≤ y ≤ 1): x goes from 0 to √y.
- Region R₂ (1 ≤ y ≤ 2): x goes from 0 to 2-y.
Step 3: Write the New Integral
I = ∫₀¹ ∫₀⁺√y xy dx dy + ∫₁² ∫₀²⁻ʸ xy dx dy
Step 4: Evaluate First Integral (I₁)
I₁ = ∫₀¹ [x²y/2]₀⁺√y dy = ∫₀¹ y²/2 dy = [y³/6]₀¹ = 1/6
Step 5: Evaluate Second Integral (I₂)
I₂ = ∫₁² [x²y/2]₀²⁻ʸ dy = ∫₁² y(2-y)²/2 dy
= (1/2)∫₁² (4y – 4y² + y³) dy
= (1/2)[2y² – 4y³/3 + y⁴/4]₁²
= (1/2)[(8 – 32/3 + 4) – (2 – 4/3 + 1/4)]
= (1/2) [ 4/3 – 11/12 ] = 5/24
Total Integral I = I₁ + I₂ = 1/6 + 5/24 = 9/24 = 3/8
Triple Integral: Calculating Volume of a Tetrahedron
Problem 9: Find the volume bounded by x=0, y=0, z=0 and x+y+z=1
Step 1: Set up the Triple Integral
Volume V = ∭∭∭ dV = ∭∭∭ dz dy dx.
The region is a tetrahedron with vertices (0,0,0), (1,0,0), (0,1,0), and (0,0,1).
Step 2: Determine Limits
- x varies from 0 to 1.
- For fixed x, y varies from 0 to 1-x.
- For fixed x and y, z varies from 0 to 1-x-y.
Step 3: Evaluate the Integral
V = ∫₀¹ ∫₀¹⁻ₓ ∫₀¹⁻ₓ⁻ʸ dz dy dx
= ∫₀¹ ∫₀¹⁻ₓ (1 – x – y) dy dx
= ∫₀¹ [(1-x)y – y²/2]₀¹⁻ₓ dx
= ∫₀¹ [ (1-x)² – (1-x)²/2 ] dx
= ∫₀¹ (1-x)²/2 dx
= (1/2) × [-(1-x)³/3]₀¹
= (1/2) × [0 – (-1/3)] = 1/6
Volume = 1/6 cubic units
Directional Derivative of φ = xyz in Normal Direction
Problem 10: Find the directional derivative of φ = xyz at P(1,1,3) in the direction of the normal to the sphere x²+y²+z²=11 at P.
Step 1: Find the Gradient of φ
φ = xyz
∇φ = (∂φ/∂x)i + (∂φ/∂y)j + (∂φ/∂z)k
∇φ = yz i + xz j + xy k
At P(1, 1, 3): ∇φ = 3i + 3j + 1k
Step 2: Find the Normal Vector to the Sphere
The sphere is defined by F = x² + y² + z² – 11 = 0.
Normal = ∇F = 2xi + 2yj + 2zk
At P(1, 1, 3): ∇F = 2i + 2j + 6k
Step 3: Find the Unit Normal Vector (n)
Magnitude: |∇F| = √(4 + 4 + 36) = √44 = 2√11
Unit vector: n = (2i + 2j + 6k) / (2√11) = (i + j + 3k) / √11
Step 4: Calculate the Directional Derivative
Directional Derivative = ∇φ · n
= (3i + 3j + 1k) · (i + j + 3k)/√11
= (3×1 + 3×1 + 1×3)/√11
= 9/√11
Directional Derivative = 9/√11 or (9√11)/11
Gauss Divergence Theorem Verification on a Cylinder
Problem 11: Evaluate ∭∭S F·n dS where F = x²i + y²j + 4zk and S is the cylinder x²+y²=4, z=0 to z=3.
Step 1: State Gauss Divergence Theorem
The theorem relates the surface integral to the volume integral of the divergence:
∭∭S F·n dS = ∭∭∭V (∇·F) dV
Step 2: Calculate Divergence (∇·F)
F = x²i + y²j + 4zk
∇·F = ∂(x²)/∂x + ∂(y²)/∂y + ∂(4z)/∂z
∇·F = 2x + 2y + 4
Step 3: Set up the Volume Integral
The volume V is a cylinder defined by r ≤ 2 and 0 ≤ z ≤ 3. We use cylindrical coordinates (dV = r dr dθ dz).
∇·F = 2r cosθ + 2r sinθ + 4
∭∭∭V (∇·F) dV = ∫₀³ ∫₀²π ∫₀² (2r cosθ + 2r sinθ + 4) r dr dθ dz
Step 4: Evaluate the Integral
Integrate r first:
∫₀² (2r² cosθ + 2r² sinθ + 4r) dr = [2r³ cosθ/3 + 2r³ sinθ/3 + 2r²]₀²
= 16 cosθ/3 + 16 sinθ/3 + 8
Integrate θ:
∫₀²π (16 cosθ/3 + 16 sinθ/3 + 8) dθ = [16 sinθ/3 – 16 cosθ/3 + 8θ]₀²π
= (0 – 16/3 + 16π) – (0 – 16/3 + 0) = 16π
Integrate z:
∫₀³ 16π dz = 16π × 3 = 48π
Answer: ∭∭S F·n dS = 48π
Verifying Stoke’s Theorem for a Square Region
Problem 12: Verify Stoke’s theorem for F = x²i + xyj around the square x=0, y=0, x=a, y=a in the z=0 plane.
Step 1: State Stoke’s Theorem
The theorem relates the line integral around a closed curve C to the surface integral over the surface S bounded by C:
∮C F·dr = ∭∭S (∇×F)·n dS
Step 2: Evaluate LHS (Line Integral ∮C F·dr)
F = x²i + xyj. Thus, F·dr = x²dx + xy dy.
The path C is the square OABCO (O(0,0) → A(a,0) → B(a,a) → C(0,a) → O(0,0)).
- Along OA (y=0, dy=0, x: 0→a):
∫OA = ∫₀ⁿ x² dx = [x³/3]₀ⁿ = a³/3 - Along AB (x=a, dx=0, y: 0→a):
∫AB = ∫₀ⁿ a y dy = a[y²/2]₀ⁿ = a³/2 - Along BC (y=a, dy=0, x: a→0):
∫BC = ∫ⁿ₀ x² dx = [x³/3]ⁿ₀ = -a³/3 - Along CO (x=0, dx=0, y: a→0):
∫CO = ∫ⁿ₀ 0 dy = 0
LHS = a³/3 + a³/2 – a³/3 + 0 = a³/2
Step 3: Evaluate RHS (Surface Integral ∭∭S (∇×F)·n dS)
Calculate the Curl (∇×F):
∇×F = yk
The surface S is in the z=0 plane, so the unit normal vector is n = k.
(∇×F)·n = yk · k = y
RHS = ∭∭S y dS = ∫₀ⁿ ∫₀ⁿ y dx dy
= ∫₀ⁿ y [x]₀ⁿ dy = ∫₀ⁿ a y dy
= a [y²/2]₀ⁿ = a³/2
Since LHS = RHS = a³/2, ✓ Stoke’s Theorem is Verified!
