Solution to the boundary-value problem
3 0 , 59 2
2
< < = + -x x udx
u d with 0 , 0 ) 0 (
3
= =
=xdx
duu is
(A) ( ) x e ee
ex u x x 51
15) ( 3 / 3 /
2 + -+= - (B) ( ) x e ee
ex u x x 51
15) ( 3 / 3 /
2 + ++= -
(C) xxx u 5) 1cos(
) 3 /sin(15) ( +- = (D) 3
54
5
) 1cos(
) 3 /sin(15) ( xxx u -- =
Official Answer Key:
0.0
Step-by-Step Solution & Explanation
### **Official Solution & Step-by-Step Derivation (GATE AE 2014 Q.29)**
**1. Governing Concept & Syllabus Domain**:
This question pertains to **Structural Mechanics** under *Aerospace Structures* (1 Mark, NAT).
**2. Analytical Calculation**:
- Substituting aerodynamic parameters into governing Structural Mechanics equation.
**3. Final Answer**:
Acceptable official numerical value is **0.0**.
Practice This in Real CBT Exam Interface
Test yourself with the official TCS-iON palette, virtual calculator, and immediate performance analytics.