AIRCRAFT AERODYNAMICS EXAM PREP
BUNDLED EXAMS WITH ACTUAL QUESTIONS
AND COMPLETE VERIFIED SOLUTIONS
ALREADY GRADED A+
◉At the aft CG limit the horizontal stabilizer and elevator . Ans: must
develop less down force to balance the decreased forward loading
◉At what airspeed will an increase in pitch attitude cause a jet to climb
while the forces along the flight path remain balanced? . Ans: an
airspeed above Vs.
◉Sweepback wing design on turbojets . Ans: delays drag rise to that
typical of slower speeds
◉How are wingtip vortices proportionately related to speed, weight, and
wingspan? . Ans: directly to weight, indirectly to speed and wingspan
BUNDLED EXAMS WITH ACTUAL QUESTIONS
AND COMPLETE VERIFIED SOLUTIONS
ALREADY GRADED A+
◉At the aft CG limit the horizontal stabilizer and elevator . Ans: must
develop less down force to balance the decreased forward loading
◉At what airspeed will an increase in pitch attitude cause a jet to climb
while the forces along the flight path remain balanced? . Ans: an
airspeed above Vs.
◉Sweepback wing design on turbojets . Ans: delays drag rise to that
typical of slower speeds
◉How are wingtip vortices proportionately related to speed, weight, and
wingspan? . Ans: directly to weight, indirectly to speed and wingspan
