ASSIGNMENT SHEET 2-2-3: LIFT PRODUCTION AND DRAG REVIEW

Descripción

This lesson is a continuation of aerodynamic principles from Lesson 2.1. Definitions of lift, weight, thrust and drag and how each relates to one another on an aircraft will be presented. Basic configuration principles and effects on lift production will also be discussed.
Justin Vaughan
Test por Justin Vaughan, actualizado hace más de 1 año
Justin Vaughan
Creado por Justin Vaughan hace más de 8 años
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Resumen del Recurso

Pregunta 1

Pregunta
Aerodynamic force is the ______.
Respuesta
  • force that is perpendicular to the relative wind
  • leading edge stagnation point
  • result of pressure and friction distribution over an airfoil
  • force that is parallel to the relative wind

Pregunta 2

Pregunta
The component of aerodynamic force that acts parallel to the relative wind is ______.
Respuesta
  • parasite drag
  • lift
  • drag
  • angle of attack

Pregunta 3

Pregunta
A ______ airfoil produces lift at zero degrees angle of attack.
Respuesta
  • symmetric
  • tapered
  • dihedral
  • positively cambered

Pregunta 4

Pregunta
L/DMAX is the point where ______.
Respuesta
  • drag is the greatest
  • lift is the greatest
  • the ratio of lift to drag is the greatest
  • the stall angle of attack is reached

Pregunta 5

Pregunta
Total drag is composed of ______.
Respuesta
  • parasite and induced drag
  • form and interference drag
  • thrust and lift
  • upwash and downwash

Pregunta 6

Pregunta
Parasite drag is ______.
Respuesta
  • the component of drag associated with the production of lift
  • minimized by installing winglets, wingtip fuel tanks or missile rails
  • greatest at low airspeeds
  • made up of form, friction, and interference drag

Pregunta 7

Pregunta
Maximum excess power for a propeller-driven aircraft occurs ______ L/DMAX.
Respuesta
  • at an airspeed below
  • at
  • at an airspeed above
  • independent of

Pregunta 8

Pregunta
As altitude increases, power available ______.
Respuesta
  • increases
  • remains the same
  • decreases
  • is equal to thrust available

Pregunta 9

Pregunta
A ______ trim tab will increase the force required to move a control surface to full deflection
Respuesta
  • servo
  • neutral
  • anti servo
  • balanced
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