A pitot probe on an aircraft in a steady, level flight records a pressure of 55,000 N/m 2. The
static pressure and density are 45,280 N/m2 and 0.6 kg/m3, respectively. The wing area and
the lift coefficient are 16 m2 and 2, respectively. The wing loading (in N/m2) on this aircraft
is _________ (accurate to one decimal place).
Official Answer Key:
0.0
Step-by-Step Solution & Explanation
### **Official Solution & Step-by-Step Derivation (GATE AE 2018 Q.43)**
**1. Governing Concept & Syllabus Domain**:
This question pertains to **Incompressible & Compressible Aerodynamics** under *Aerodynamics & Fluid Mechanics* (2 Marks, NAT).
**2. Analytical Calculation**:
- Substituting aerodynamic parameters into governing Incompressible & Compressible Aerodynamics 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.