AFOQT EXAM NEWEST ACTUAL QUESTIONS WITH

AFOQT EXAM NEWEST ACTUAL / QUESTIONS WITH

100% CORRECT ANSWERS VERIFIED /GRADED A+

reactants/reagents of combustion reaction - ---Answers---- oxygen reactant/ water and carbon dioxide products

extrinsic properties of matter - ---Answers----related to the amount of material used (mass/volume)

a - ---Answers----Profile drag is the sum of:

(A) Skin friction and form drag (B) Skin friction and induced drag (C) Form drag and supplementary drag (D) Parasite drag and vortex drag

d - ---Answers----Slats are located:

(A) Along the horizontal stabilizer's leading edge (B) Along the leading edge of both wings and the horizontal stabilizer.(C) Along the trailing edge of the right aileron (D) Along the leading edge of both wings

d - ---Answers----The laws of conservation that pertain to

aircraft are:

(A) The law of conservation of mass, kinetic energy, and fluid flow. 1 / 4

(B) The law of conservation of mass, torque, and potential energy.(C) The law of conservation of weight, thrust, and lift.(D) The law of conservation of mass, energy, and momentum.

b - ---Answers----Parasite drag is produced by:

(A) Extended slats and flaps (B) Aircraft parts that do not contribute to producing lift (C) Improperly set trim tabs (D) A difference in propeller rpm on multi-engine airplanes

b - ---Answers----The angle of attack is:

(A) The chord line's orientation in relation to the aircraft's longitudinal axis.(B) The acute angle between the chord line of an airfoil and the relative wind.(C) The sum of the angle of incidence of the wings and tailplane.(D) The aircraft's downward inclination when shooting targets on the ground.

b - ---Answers----According to 18th century Swiss scientist

Daniel Bernoulli:

(A) Accelerated fluid flow results in a decrease of dynamic pressure. 2 / 4

(B) Accelerated fluid flow results in a decrease of static pressure.(C) Accelerated fluid flow results in an increase of total system energy.(D) All of the above.

c - ---Answers----Lift produced by an airfoil is proportional

to:

(A) The rate of air compressibility and the coefficients of lift and drag.(B) The angle of airflow deflection, the relative wind's vertical vector component, and the reduction of induced drag as the aircraft accelerates.(C) Air density, aircraft speed, wing area, and airfoil shape.(D) None of the above

a - ---Answers----Thrust opposes:

(A) Drag (B) Rudder deflection (C) Gyroscopic precession (D) Gravity

a - ---Answers----Ailerons move:

(A) In opposing directions (B) Downward 3 / 4

(C) Up or down, depending n the rudder pedal pushing by the pilot (D) None of the above

c - ---Answers----The main types of turbine propulsion are:

(A) Axial and centrifugal flow (B) Non-afterburning, after-burning, and turbocharged (C) Turbofan, turbojet, and turboprop (D) Turbocharged, turbofan, and ramjet

c - ---Answers----An aircrafts three axes are:

(A) Longitudinal, gyroscopic, and lateral (B) Directional, pitch, and gyroscopic (C) Yaw, longitudinal, and lateral (D) Deflectional, lateral, and induced

b - ---Answers----Increasing an aircraft's bank in a

coordinated turn, ______ its ______ and ______:

(A) increases; angle of attack; lift (B) increases; weight (due to "G" loading); rate of turn (C) decreases; angle of attack; drag (D) decrease; weight (due to "G" loading); angle of attack

a - ---Answers----When a pilot pulls back on the control

column or joystick:

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