PROJECT 2: Fortran Programming

Part 2c
Problem Statement

Determine ground roll takeoff distance required on a dry runway at sea-level for a Boeing 767-like aircraft using:
a) the spline & intergration subroutines of Projects 2a) and 2b).
b) the simplified approach ( assumes avg. accel.=1/(A+B*V**2/2))

Aircraft Characteristics

T/O Weight387,000 lb
Wing Planform Area3084 sq ft
Wing Span156.1 ft
f127.5 sq ft
Wing Span156.1
Oswald Efficiency.7
Ground Effect factor.4
CL (full flaps)1.0
VLO145 kt
Rolling Friction.03
 

ENGINE CHARACTERISTICS

SPEEDTHRUST
fpspounds
055600
2554472
3853904
55 53178
8352028
10551164
13350113
15649293
18148444
21547360
25046331

Submit

  1. source codes
  2. include files
  3. input files
  4. plot of distance vs time for a)& b)
  5. plot of speed vs time for a)& b)
  6. compare results for a) & b)

Due:Feb 9, 10AM