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Military

AL0966 Practice Exercise
Lesson 1,2 & 3: Basic Aerodynamics

Instructions The following items will test your understanding of the material covered in lessons 1, 2, and 3. There is only one correct answer for each item. When you have completed the exercise, check your answers with the answer key that follows. If you answer any item incorrectly, review that part of the lesson which contains the portion involved.  

True - False

Select True or false for the following questions.


  1.   On an aircraft having aerodynamically clean characteristics, speed brakes are used to improve the rate of ascent.

True
False
  2.   The surfaces of a wing or rotor blade are designed to produce lift when air passes over it. Two-thirds of the lift is produced by the lower pressure air passing over the wing's or blade's upper surface.

True
False
  3.   The rotor system is using from 20 to 100 percent of the available power and the horizontal velocity is 10 knots or less. Under this condition a pilot may experience settling with power.

True
False
  4.   The lateral axis runs from wing tip to wing tip.

True
False
  5.   The man who first sketched the helicopter and referred to it as a helixopteron was Giovanni Venturi.

True
False
  6.   Sir Isaac Newton's third law of motion is: for every action there is an equal and opposite reaction.

True
False
  7.   Improved lift and airfoil efficiency while operating in ground effect are due to the recirculation of the main rotor tip vortex.

True
False
  8.   The term "standard conditions" refers to atmospheric pressure of approximately 14.7 psi or 29.92 inches of mercury at sea level with a temperature of 15°C.

True
False

Cluster True - False

NOTE:  (Each question of this kind consists of a series of statements related to the stem that precedes them. Select True or False for each question.)

 
  9.   A given volume of dry air contains a variety of gases representative of the earth's atmosphere. Indicate which of the following statements most accurately states the composition of this variety.
        a.  Nitrogen, oxygen, argon, carbon dioxide, and minute amounts of other gases.

True
False
        b.  Water vapor, dust, and salt particles.

True
False
        c.  A percentage of gases varying with the temperature of the air.

True
False
        d.  One percent of other gases, 21 percent oxygen, and 78 percent nitrogen.

True
False
        e.  Fifty percent oxygen, 48 percent nitrogen, and 2 percent argon.

True
False
Matching

  10.   Match the statements in column I with the terms to which they apply in column II. Items in column II may be used once, more than once, or not at all.

Column I

Column II

(1)  Control surfaces in the empennage group.

A.  B.  C.  D.  E.  F.  G. 

  1. Chord line.

  2. Rudder an elevator.

  3. Ailerons.

  4. Flaps, aileron, tail rotor.

  5. Cyclic, collective pitch and antitorque.

  6. Rudder.

  7. Center of gravity line
(2)  An imaginary line drawn from the center of the leading edge to the trailing edge of an airfoil.

A.  B.  C.  D.  E.  F.  G. 

(3)  Three basic controls in a helicopter

A.  B.  C.  D.  E.  F.  G. 

(4)  Control an aircraft about its bank or roll axis.

A.  B.  C.  D.  E.  F.  G. 

 

Multiple Choice

NOTE: (Each question in this group contains one and only one correct answer. Make your choice by selecting the proper letter for each question.)

  11.   The blade element located between approximately 25 and 75 percent radius is known as the auto-rotative or driving region.

A. This region operates at a negative angle of attack and has no effect.
B. This region operates at a comparatively high angle of attack.
C. This region operates at a complete stall angle of attack.
D. This region operates at a comparatively low angle of attack.
  12.   An airfoil's angle of attack is measured between the.

A. Aircraft fuselage and the empennage group.
B. Wing root and the wing tip.
C. Airfoil chord and the relative wind.
D. Angle of airfoil and the airstream.
  13.   The average temperature lapse rate is:

A. Based on the worldwide variation of temperatures with altitude.
B. Dependent upon weather over land or sea.
C. Measured in degrees of change per kilometer.
D. Affected by the height of the stratosphere and time of year.
  14.   Gyroscopic precession is the result of a force applied against a rotating body, and it occurs, approximately, at a point:

A. Two hundred and seventy degrees later in the direction of rotation from the point where the force is applied.
B. One hundred and twenty degrees opposite that of rotation from the point where the force is applied.
C. Ninety degrees later in the direction of rotation from the point where force is applied.
D. One hundred and eighty degrees out of phase from the point where force is applied.
  15.   If the pressure altitude is 7,000 feet and the temperature is +15°C the density altitude is:

A. 9,800.
B. 7,200.
C. 8,600.
D. 6,500.
  16.   A wing that has no external supports is called a:

A. Cantilever wing.
B. Symmetrical wing.
C. Wing chord.
D. Laminate wing.
  17.   Lift, weight, thrust, and drag are the four forces that act on an aircraft. You are correct in making which of the following statements.

A. Induced and parasite are two types of drag forces.
B. On a conventional aircraft, the propeller or jet engine is used to overcome gravity.
C. The four forces must be unequal to maintain straight and level flight.
D. Only the weight of the aircraft and its fuel must be against gravity.
  18.   When the helicopter is moving forward at a speed of 150 knots, and the velocity of the rotor blade tip is 363 knots, the advancing and retreating blade speeds are:

A. 513 and 213 knots.
B. 513 and 313 knots.
C. 531 and 213 knots.
D. 531 and 231 knots.