Aerospace Engineering > GATE 2018 > Aircraft Performance
A pitot probe on an aircraft in a steady, level flight records a pressure of 55,000 N/m2 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).
Correct : 18000 to 19440
Similar Questions
Which one of the following figures represents the drag polar of a general aviation aircraft?
Which of the following statements about a general aviation aircraft, while operating at point Q in the V-n diagram, is/are true?
An airplane experiences a net vertical ground reaction of 15000 N during landing. The weight of the airplane is 10000 N. The landing vertical load factor, defin...
Total Unique Visitors
Loading......