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Find positive limit load and positive ultimate limit load

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Reference no: EM13574160

Conditions:

  • W=10,000 lb
  • S = 100 ft2
  • CLMAX = 1.5

Aircraft Certified Aerobatic Category (-3, +6) G

1. Find Stall Speed (KEAS) at 1 G, 0 deg AOB.

2. Find Stall Speed (KEAS), level flight 70 deg AOB (2.9 G).

3. Find Positive Limit Load and Positive Ultimate Limit Load of Given Aerobatic Aircraft-Max Gross Weight = 10,000 lb.

4. Find Maneuvering speed (Va) of given aerobatic aircraft W=10,000 lb.

5. Find Turn Radius and Rate of Turn of aerobatic aircraft performing level sustained 4 G turn at 100 KTAS.

6. Using Figure 14.10 from Flight Theory and Aerodynamics, find AOB to fly a standard rate turn (3 deg/sec) at 200 KTAS.

7. Name four different design features for supersonic aircraft.

8. What is rate of turn and turn radius of Pitts doing 3g turn at 110 imph (indicated statute miles per hour)? Compare your mathematical answer of turn rate to that of the aircraft aviation video link (Time the 3 g turn of 360 deg and then divide by 360 to get deg/sec)?

Reference no: EM13574160

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