AE 332

CSRJ 150

WEIGHTS AND RANGE

• Operational Empty Weight =36 ton
• Maximum Take-Off Weight = 63 ton
• Maximum Landing Weight = 60 ton
• Maximum Zero Fuel Weight = 60 ton
• Range = 3254 nm
• Wing Area = 120 square meters
• Fuel Capacity = 20 ton

CSRJ 180

• Operational Empty Weight =43 ton
• Maximum Take-Off Weight = 75 ton
• Maximum Landing Weight = 71 ton
• Maximum Zero Fuel Weight = 70 ton
• Range = 3197 nm
• Wing Area = 120 square meters
• Fuel Capacity = 20 ton

CABIN

FAR 25 Regulations

Emergency Exits Every 30 feet on Each Side

• TYPE B EXITS IN FRONT AND AFT
• TYPE I EXITS OVER THE WING

FRIEGHTER???

Perfectly Circular Crossection

LD3-45 Containerized Cargo Bay

Thrust to Weight = 0.32

CONSTRAINTS:-

THRUST AND WING

• Second Segment Climb = 0.27(0.3 rho penalty)
• Missed Approach Climb Gradient = 0.29(0.3 rho penalty)

CFM LEAP

10:1 Bypass Ratio

16% Lower Fuel Consumption

• Cruise Speed = 828 KMPH = 0.78M AT 35000ft
• Cruise CL = 0.48
• CLmax = 2.69
• Landing Field Length = 2130m
• Take-off Field Length = 1855m
• Vapproach = 140 kts

PERFORMANCE ESTIMATES FOR CSRJ 150

WING SPECIFICATIONS

• Type C Gate
• Span = 35.6m
• Area = 120 sq.m
• Taper Ratio = 0.3
• Sweep = 25 deg
• Aspect Ratio = 10.5
• Wing Loading = 525 kg/sq.m on the CSRJ 150
• = 625 kg/sq.m on the CSRJ 180

WING CONSTRAINTS:-

• Wing Area From Stall Speed > 106sq.m
• Wing Area From Cruise < 120sq.m

• Cruise Speed = 828 KMPH = 0.78M AT 35000ft
• Cruise CL = 0.57
• CL_max = 2.69
• Landing Field Length = 2450m
• Take-off Field Length = 2260m
• V_approach = 153 kts

PERFORMANCE ESTIMATES FOR CSRJ 180

32 inch Seat Pitch

SEAT PITCH 32 INCH

1591 ft^3

Range

3200 nm

3060 nm

9LD3-46

Cargo Capacity

Group A

Presents

Notional 3 Veiw Diagram With Scale Wing, Fuselage and Cabin

Take-off Length

32 in (Typical)

30 in (Dense)

Seat Pitch

2400 m

2100 m

Passenger Comfort

Seat Width

17.5 in

CSRJ

189(1 class dense)

175 (typical 1 class)

160 (2 class)

Seat Capacity

150-180 typical

Approach Speed

142 kts

Fuel Burn per

Passenger mile

140 kts

0.035(20% improvement)

0.0465

DR&O

$2.0 trillion :)

By 2031, total single aisle fleet share will rise to 69%

MARKET SURVEY RESULTS

Reference:SUGAR NASA

Asia Pacific region is expected to need 7,990 new airplanes to expand its single-aisle by 2031!!!

Ankit Shah (09001006)

Nishant Khanduja (09001013)

Gaurav Tendolkar (09D01003)

Utkarsh Vijay (09D01012)

Satwik Pradhan (09001020)

Seng Sy Keath (12V011001)

Prateek Jolly(P11314)

Single-aisle airplanes will continue to dominate the world’s fleet

Layout Showing Control Surfaces and Wing Spars

• Span = 11.9 m
• Root Chord = 3.9 m
• Tip Chord = 0.861 m
• Sweep = 30deg
• Area = 24.48sq.m

Horizontal Tail

Extreme Lower Static Margin = 5% MAC

C.G. Travel = 30% MAC

Tail Arm = 45% of Fuselage Length

Neutral Point and C.G.

Same tail on the CSRJ 150 and the CSRJ 180!!

TAIL SIZING, NEUTRAL POINT & C.G.

• Span = 6.935 m
• Root Chord = 4.172 m
• Tip Chord = 1.378 m
• Sweep = 40deg
• Area = 19.24sq.m

Vertical Tail

Cost of Aircarft = $75 Million

all dimensions in meters

Neutral point

Aftmost C.G.

Empty C.G.

Wing A.C.

Forwardmost C.G.

Nose Gear - 4108 Pounds

Oleo Diameter - 2.2 inch

Main Gear - 95% Load - 4 Wheels per Gear

Nose Gear - 5% Load - 2 Wheels per Gear

Front Spar at 15% from local L.E.

Rear Spar 65% from Local L.E.

Oleos for Landing Gear

Main Gear - 22000 Pounds

Oleo Diameter - 5.1 inch

STRUCTURES AND COST

Take off CL_max with 20 deg Flaps = 2.4

Landing CL_max with 35 deg Flaps = 2.69

• Single Slotted Flaps With High Fowler Motion
• Leading Edge Slats

High Lift Systems

Untrimmed L/D vs CL

Span Variation For Optimum L/D

Drag Breakup for CSRJ 180

AERO DATA