At what angle should the plane be flown at to maximize the range?

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?

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