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Tony's Intertwingled Memex • Reference Manual

Aerospace Engineering (Structural Integrity under Thermal Expansion) Solution

Formulas & Definitions

Problem Overview

We calculate the second derivative d2ydx2\frac{d^2y}{dx^2}dx2d2y​ along an implicit circular viewport:

x2+y2=25x^2 + y^2 = 25x2+y2=25
evaluated at the coordinate point (x,y)=(3,4)(x, y) = (3, 4)(x,y)=(3,4) to determine localized curvature and concavity under thermal expansion stress.


Step-by-Step Mathematical Solution

Step 1: Find the First Derivative dydx\frac{dy}{dx}dxdy​

Differentiate both sides with respect to xxx:

ddx[x2]+ddx[y2]=ddx[25]\frac{d}{dx}[x^2] + \frac{d}{dx}[y^2] = \frac{d}{dx}[25]dxd​[x2]+dxd​[y2]=dxd​[25]
2x+2ydydx=0  ⟹  dydx=−xy2x + 2y\frac{dy}{dx} = 0 \implies \frac{dy}{dx} = -\frac{x}{y}2x+2ydxdy​=0⟹dxdy​=−yx​
(This rule is defined in Implicit Differentiation.)

Step 2: Differentiate a Second Time Using the Quotient Rule

Apply the Quotient Rule to dydx=−xy\frac{dy}{dx} = -\frac{x}{y}dxdy​=−yx​:

d2ydx2=ddx[−xy]=−[ddx[x]⋅y−x⋅ddx[y]y2]=−y−xdydxy2=−y+xdydxy2\frac{d^2y}{dx^2} = \frac{d}{dx}\left[-\frac{x}{y}\right] = -\left[ \frac{\frac{d}{dx}[x] \cdot y - x \cdot \frac{d}{dx}[y]}{y^2} \right] = -\frac{y - x\frac{dy}{dx}}{y^2} = \frac{-y + x\frac{dy}{dx}}{y^2}dx2d2y​=dxd​[−yx​]=−[y2dxd​[x]⋅y−x⋅dxd​[y]​]=−y2y−xdxdy​​=y2−y+xdxdy​​

Step 3: Back-Substitute dydx=−xy\frac{dy}{dx} = -\frac{x}{y}dxdy​=−yx​

d2ydx2=−y+x(−xy)y2=−y−x2yy2\frac{d^2y}{dx^2} = \frac{-y + x\left(-\frac{x}{y}\right)}{y^2} = \frac{-y - \frac{x^2}{y}}{y^2}dx2d2y​=y2−y+x(−yx​)​=y2−y−yx2​​

Step 4: Clear Fractions and Substitute Original Equation Constraint

Multiply numerator and denominator by yyy:

d2ydx2=−y2−x2y3=−(x2+y2)y3\frac{d^2y}{dx^2} = \frac{-y^2 - x^2}{y^3} = \frac{-(x^2 + y^2)}{y^3}dx2d2y​=y3−y2−x2​=y3−(x2+y2)​
Because the curve is constrained by x2+y2=25x^2 + y^2 = 25x2+y2=25:
d2ydx2=−25y3\frac{d^2y}{dx^2} = -\frac{25}{y^3}dx2d2y​=−y325​
(This technique is detailed in Higher-Order Implicit Differentiation.)

Step 5: Evaluate at (3,4)(3, 4)(3,4)

Substitute y=4y = 4y=4:

d2ydx2∣(3,4)=−2543=−2564≈−0.3906 cm−1\left.\frac{d^2y}{dx^2}\right|_{(3,4)} = -\frac{25}{4^3} = -\frac{25}{64} \approx -0.3906\text{ cm}^{-1}dx2d2y​​(3,4)​=−4325​=−6425​≈−0.3906 cm−1


Engineering Conclusion

Because d2ydx2=−2564<0\frac{d^2y}{dx^2} = -\frac{25}{64} < 0dx2d2y​=−6425​<0, the bulkhead viewport edge is strictly concave downward at (3,4)(3, 4)(3,4). In aerospace structural engineering, geometric curvature (κ=∣y′′∣(1+(y′)2)3/2\kappa = \frac{|y''|}{(1 + (y')^2)^{3/2}}κ=(1+(y′)2)3/2∣y′′∣​) determines the severity of stress concentrations. If localized heating causes a boundary to buckle beyond its material curvature allowance, high shear stresses can crack silica glass viewports. Knowing that d2ydx2=−2564\frac{d^2y}{dx^2} = -\frac{25}{64}dx2d2y​=−6425​ enables stress analysts to verify that the titanium retaining ring distributes re-entry pressure loads evenly around the seal.