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EG2100 Engineering Design II - Aerospace (PRD1 A 2025/26)
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NOTE: DO NOT MOVE ON TO THE NEXT PAGE WITHOUT ATTEMPTING THESE THREE QUESTIONS!
Consider an aircraft with the following aerodynamic & mission specification:
CD0 = 0.0173; k = 1.22; AR = 9.3
Cruise Mach = 0.78 at 34,000 ftThrottle setting 75%
Cruise weight = 0.96 % MTOW
Residual rate of climb allowance = 2.0 m/s
Answer the following three questions in turn:
Q1 What is the density of the atmosphere at the cruise altitude, in kg/m3 , to 4 d.p.?