Aerospace Fundamentals
Short Answer Questions (5 Points Each):
1. Briefly discuss the function of the following components in a gas turbine engine:
a. Turbine
b. Burner
c. Compressor
2. 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?
3. A glider has a maximum lift to drag ratio of 30. At what angle should the plane be flown at to maximize the range?
4. 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?
