Aerospace Fundamentals
Short Answer Questions (5 Points Each):
Briefly discuss the function of the following components in a gas turbine engine:
Turbine
Burner
Compressor
A new engine design is capable of providing a fighter aircraft with 40% more excess power and weighs 10% less – all else being equal. By what percentage has the rate of climb increased?
A glider has a maximum lift to drag ratio of 30. At what angle should the plane be flown at to maximize the range?
Shown below is the F-14 aircraft in two different wing sweep configurations. What are the benefits to wing sweep at subsonic and supersonic speeds?
Briefly discuss the function of the following components in a gas turbine engine. Explain what are the benefits to wing sweep at subsonic and supersonic speeds?
