Aero 242             INDIVIDUAL FINAL PROJECT 2             S99
3/25/99

Objective

Create a Range Payload plot for the aircraft given by the configuration file below:

ConfigurationMissionOutput
19350 W0
318 S
8.9 AR
.81 E
.02 Cdo
1.8 Clmax
2 Neng
4000 Tmax
3650 Tasl
.6 TSFC
5500 MaxPay
 
5000 Horigin
4000 Sorigin
0.02 MUorigin
38000 Hcr
.64 Mcr
2500 Rcr
10000 Hloit
50 Endur
40000 Sceil
0 Hdest
6000 Sdest
0.4 MUdest
 
Wempty
Wpay
Wfuel
Sceil
Mcr
Vloit
Sdest
Sorigin
Tcruise

Requirements

  1. Add a take-off routine for total runway requirement over a 100 foot obstacle
  2. Add a landing routine for total runway requirement over a 30 foot obstacle
  3. Add a service ceiling routine
  4. Keep all of the configuration variables fixed.
  5. Vary only Mcr and Rcr to determine Wpay
    All other mission constraints are fixed.
Note: The design payload should be Wpay = 3700 lb (approx) and Mcr = 0.64 (approx)