Wing Loading MCQ

Test your knowledge with important Wing Loading MCQ and their applications. These MCQs are beneficial for competitive exams too. Explore 30 + more Wing Loading MCQs at Bissoy

• An aircraft has catapult end speed of 30m/s and wind over deck as 20m/s. If maximum CL is 2.6 and density is 1.22 then, find catapult wing loading.
  ক

  3276.859

  খ

  327

  গ

  32

  ঘ

  2
• Following graph represents __________
  ক

  take-off distance estimation

  খ

  take-off velocity

  গ

  wing loading

  ঘ

  power loading
• Determine wing loading for civil aircraft if lift-off speed is 80m/s and maximum lift coefficient is 2.8.
  ক

  9071.07

  খ

  9111

  গ

  911

  ঘ

  91
• As a designer I want to reduce the empty weight of my aircraft. Therefore I will ______
  ক

  increase wing loading

  খ

  decrease wing loading

  গ

  wing loading has no effect

  ঘ

  will reduce by exactly half
• Low wing loading will provide ___________
  ক

  more space for fuel storage in wing

  খ

  more space of fuel storage in cabin

  গ

  less fuel storage

  ঘ

  less lift
• Design lift coefficient is determined by wing loading.
  ক

  True

  খ

  False
• Wing loading will affect _____________
  ক

  only stall speed

  খ

  only ground roll

  গ

  stall speed, climbing, ground roll etc

  ঘ

  only climb
• Wing loading is ratio of ___________
  ক

  weight of the aircraft and the reference area of wing

  খ

  reference area of wing and power of engine

  গ

  lift to drag

  ঘ

  aerodynamic force thrust to drag