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Technical question and answer ( CPL ) Dgca exam CA$11.71   Add to cart

Exam (elaborations)

Technical question and answer ( CPL ) Dgca exam

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Quiz used for technical exam conducted by DGCA . It is referred from Oxford book Principle of flight.

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  • April 20, 2023
  • 6
  • 2022/2023
  • Exam (elaborations)
  • Questions & answers
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TECHNICAL GENERAL (CPL) USAV104 F.Y.B.Sc Aviation University Of
Mumbai Q&A Practice Quiz


1. The angle between the aeroplane longitudinal axis and the chord line is the:
• Angle of incidence


2. Maintaining thickness/chord ratio but changing to a supercritical wing section will:
• Give the aircraft an increased range


3. Assuming ISA conditions, which statement with respect to the climb is correct?
• At constant IAS the Mach number increases


4. The point about which the wing pitching moment is independent of angle of attack is
called
• The aerodynamic centre


5. The unit of measurement of pressure is:
• psi


6. The unit of density is:
• kg/m3


7. The angle of attack of a wing profile is defined as the angle between:
• The undisturbed airflow and the chordline


8. Wing loading is:
• The ratio of aircraft weight to wing area

, 9. The term angle of attack is defined as:
• The angle between the wing chord line and the relative wind


10. At a constant IAS, induced drag is affected by:
• Aircraft weight


11. What is the effect on EAS as height is increased when you are holding a constant IAS?
• EAS falls


12. At a constant CAS when flying below sea level an aircraft will have:
• A lower TAS than at sea level at ISA conditions


13. The angle of attack of a two dimensional wing section is the angle between:
• The chord line of the aerofoil and the free stream direction


14. The units of wing loading and dynamic pressure q are:
• N/m2


15. What is the MAC of a wing?
• The same as the mean chord of a rectangular wing of the same span


16. A symmetrical aerofoil section at CL = 0 will produce?
• Zero pitching moment


17. The CP on a swept wing aircraft will move forward due to:
• Up stall of the wing

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