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:
Configuration Mission Output
19350 W0 
318  S 
8.9  AR 
.81  E 
.02  Cdo 
1.8  Clmax 
.2  Clto 
0  Clland 
2  Neng 
4000 Tmax 
3650 Tasl 
0 Trev 
.6 TSFC 
5500 MaxPay 
500 MinPay 
 
5000 Horigin 
0.02  MUorigin 
38000 Hcr 
.64  Mcr 
2500 Rcr 
10000  Hloit 
50  Endur 
0  Hdest 
0.4  MUdest
1.2  npullup 
 
Wempty
Wpay
Wfuel 
ServCeil
Mcr
Vloit
Sdest
Sorigin 
Tcruise

Requirements

  1. Add a take-off routine for total runway requirement over a 35 foot obstacle
  2. Add a landing routine for total runway requirement over a 50 foot obstacle
  3. Add a service ceiling routine: use GTOW (i.e.,W0)
  4. Keep all of the configuration variables fixed except W0 which

    5. must be changed for ranges larger than the design range.
  5. Vary only Mcr and Rcr to determine Wpay for ranges smaller than the design range.

    6. All other mission constraints are fixed.
  6. The output file should contain the variables shown as a minimum.
  7. Determine sufficient results to be able to plot a Payload/Range plot.
  8. Create a separate output file to add the output range and payload values as they are determined.
Note: The design payload should be Wpay = 2300 lb (approx) and Mcr = 0.64 (approx)

Submit

  1. Range/Payload plot which show calculated points.
  2. All input and output files at MaxPay, MinPay, Rcr = 2500 nm.
  3. "Mission" copies for MaxPay, MinPay, Rcr = 2500 nm.
  4. Your source code
Note: Copy your files, etc to a word processor for nice layout.

 

 

Due: Apr. 29, 1999