Reference no: EM13849990

One of the requirements for this course is an Aircraft Performance Research Project that entails planning a flight from Denver International Airport (KDEN) to Chicago O'Hare International Airport (KORD) for a given aircraft, weather conditions, and assumptions. The objective is to apply what has been learned throughout this course.

Drawing on aeronautics theory and using the performance charts and equations presented in the course, each student is to answer a sequence of questions that step through the planning process. Remember, as with all of the exercises, all work (calculations) must be shown as much as possible.

After all of the questions have been answered, the next task is to create a two-dimensional representation of the flight path showing the airspeeds, distance, fuel burned, and fuel remaining for the Takeoff, Climb, Cruise, Descent, and Approach phases of the flight.

Aircraft Information
Aircraft	C-9B
Engines	Twin JT8D-9 engines rated at 14,500 lb static sea level
Max Ramp Gross Weight	111,000 lb
Max Takeoff Gross Weight	110,000 lb
Max Landing	99,000 lb
Empty Weight Including Aircrew	60,000 lb
Estimated Wing Area	1300 ft2
Glide Ratio at (L/D)max	17/1
Max Fuel	38,000 lb
Max Passengers	90

Assumptions
Start/Taxi Fuel	300 lb
Takeoff Fuel Burn	700 lb
Approach Fuel Burn	300 lb /approach
Average Weight per Passenger including Baggage	225 lb/per person
Fuel Required	Start/Taxi Fuel +Takeoff Fuel + Climb Fuel + Cruise Fuel + Descent Fuel + Approach Fuel + 30 min reserve at Cruise Speed/Fuel Flow
KDEN Denver International Airport and Weather Information
Winds	160 deg @ 20 kts
Barometric Altimeter Setting	29.32
Temperature	+30 deg
KORD Chicago International Airport and Weather Information
Winds	320 deg @ 25 kts
Barometric Altimeter Setting	30.52
Temperature	0 ºC
Winds and Temperature Aloft
Cruise FL350 Winds	240 deg @ 100 kts Temperature Standard
Climb-Assume	No Winds & Temperature is ISA +15 ºC for the Climb

SECTION 1:

1.1.  Find Maximum Takeoff Weightfor the given conditions.Assume takeoff is at Max Recommended Takeoff weight accounting for Density altitude.

1.2.  Find Takeoff Speeds: V1, V2, VR. Assume Min Speed due to VMCG Requirements is OK.

1.3.  Find Flap Retraction Speed (KIAS).

1.4.  Find Slat Retraction Speed (KIAS).

1.5.  Find Critical Field Length (ft).

1.6.  Find Distance to Accelerate and Stop with a Single Engine Failure at V1 (ft).

1.7.  Find Distance to Liftoff with Single Engine Failure at V1 and continue Takeoff(ft).

1.8.  Find Two Engine Takeoff Ground Roll (ft).

1.9.  Is the runway long enough at KDEN to safely takeoff?

SECTION 2:

2.1.  Find Climb Schedule (Airspeed/Mach to be flown in the Climb).

2.2.  Find Time to Climb (min).

2.3.  Find Distance to Climb (nm).

2.4.  Find Fuel for Climb (lb).

SECTION 3:

Note. Assume no anti-ice and two engines.

3.1.  Find Cruise Indicated Airspeed (KIAS).

3.2. Find Cruise True Airspeed (KTAS).

3.3. Find Cruise Ground Speed (KGS).

3.4. Find Total Cruise Fuel Flow (lb/hr). Note, fuel flow listed is for each engine.

3.5. Find Cruise Mach (M).

3.6. Find Cruise Specific Range (nm/1000lb).

3.7. Find Maximum Level Flight Speed: Max Thrust at the Top of Climb Weight.

SECTION 4:

4.1. Find Decent Schedule (Airspeed/Mach to be flown in the Descent).

4.2. Find Time to Descent (min).

4.3. Find Fuel for Descent (lb).

4.4. Find Distance for Descent (nm).

SECTION 5:

5.1. Find Max endurance and holding speed for aircraft at GW 75k lb @10k ft Pressure Altitude.

SECTION 6:

6.1. Find Maximum passengers/baggage and fuel required for flight.

Hint: Find fuel for each segment of the flight plus reserves, and then subtract from Max Recommended Takeoff weight determined in Section 1. Then divide allowable Weight by passenger Cargo Weight.

6.2. Find Reference Speed for predicted Landing Weight (KIAS).

6.3. Find Final Approach speedwith 50 deg flaps (KIAS).

6.4. Find Landing DistanceFull Anti-Skid/ No Reverse Thrust/Full Spoilers(ft).

6.5. Find Max Angle of Bankfor Stick Shaker at Vref +5 for predicted Landing Weight.

SECTION 7:

7.1. Find Cruise FL350 Target Pitch Attitude and %N1.

7.2. Find Descent Profile.

7.3. Find Terminal Area Flight Profile (0 deg Flaps).

7.4. Find Final Approach Profile (50 deg Flaps).

SECTION 8:

8.1. Find average takeoff acceleration using takeoff ground roll and VR. (Hint. Convert VR to KTASand then to Ground Speed.)

8.2. Find average drag on takeoff roll assuming constant thrust. Account for reduced thrust at higher density altitude: Use Equation 6.5, let x = 0.8, and constant rolling friction.

Assume no lift on wings until rotation.

8.3. Find Stall Speed (KIAS) at Takeoff weight with flaps at 15 deg and slats extended.

8.4. Find CLMAX at Takeoff weight with flaps at 15 deg and slats extended.

8.5. Find Stick Shaker Speed (KIAS) at Takeoff weight with Flaps at 15 deg and slats extended.

8.6. Find CL at Stick Shaker Speed with flaps at 15 deg and slats extended.

8.7. Find Airspeed Envelope Maximum and Minimum Mach for Wings Level, GW 80,000 lb, and FL350 based on Buffet Boundary.

8.8. Find Maximum Load factor (g) and AOB at FL350 and GW 80,000 lb for buffet free flight.

8.9. Find Initial Climb Gradient for Takeoff Conditions fora single engine.

8.10. Find Initial Rate of Climb for a single-engine takeoff

8.11. Find Excess Thrust (lb) for initial single engine climb. Assume V= 1.23 Vs and V is converted to TAS.

8.12. If both engines flameout at FL350 125 nm prior to Chicago, and you fly at best glide speed, will you make Chicago on a flameout approach?

8.13. Find Drag (Thrust Required) at (L/D)max at Sea Level Takeoff weight.

8.14. Find Temperature Ram Rise at Cruise Mach for a standard temperature probe assuming 100% recovery.