- #1
aero_student
- 1
- 0
- Homework Statement
- I've tried my best to put in the correct dimensions, and my output said I needed SHB, SEXT, AND RLPH. How do I get these values? I've looked in the manual but it doesn't really say how to get those values (I also don't know how to find the mach lines).
- Relevant Equations
- DATCOM
Code:
CASEID MACH 0.5
DIM M
$FLTCON NMACH = 1.0, MACH(1)=0.50,
NALPHA = 6.0, ALSCHD(1) = -5.0, 0.0, 5.0, 10.0, 15.0, 20.0,
NALT = 3.0, ALT(1) = 0.0, 5000.0, 10000.0, WT = 2287.0, LOOP = 3.0$
$SYNTHS XCG = 5.3, ZCG = 0.0, XW = 4.0, ZW = 0.25, XH = 8.5,
ZH = 0.25, XV = 8.5, ZV = 0.25$
$BODY NX = 10.0,
X(1) = 0.0, 1.0, 2.0, 3.0, 4.0, 5.0, 6.0, 7.0, 8.0, 9.0, 10.6,
S(1) = 0.1, 0.36, 0.5, 0.5, 0.5, 0.5, 0.5, 0.5, 0.7, 0.7, 0.7$
$WGPLNF CHRDTP = 0.375, CHRDR = 1.25, SSPN = 0.625, SSPNE = 0.375,
SAVSI = 45.0, CHSTAT = 0.25, TWISTA = 0.0, DHDADO = 0.0, TYPE = 1.0$
$HTPLNF CHRDTP = 0.370, CHRDR = 1.7, SSPN = 1.0, SSPNE = 0.75,
SAVSI = 45.0, CHSTAT = 0.25, TWISTA = 0.0, DHDADO = 0.0, TYPE = 1.0$
$VTPLNF CHRDTP = 0.370, CHRDR = 1.7, SSPN = 1.0, SSPNE = 0.75,
SAVSI = 45.0, CHSTAT = 0.25, TYPE = 1.0$
NACA-W-6-66-009
NACA-H-6-66-009
NACA-V-6-66-009
PLOT
SAVE
NEXT CASE
CASEID MACH 1.5
$FLTCON NMACH = 1.0, MACH(1) = 1.5,
NALPHA = 6.0, ALSCHD(1) = -5.0, 0.0, 5.0, 10.0, 15.0, 20.0,
NALT = 3.0, ALT(1) = 0.0, 5000.0, 10000.0, WT = 2300.0, LOOP = 3.0$
PLOT
SAVE
NEXT CASE
CASEID MACH 2.5
$FLTCON NMACH = 1.0, MACH(1) = 2.5,
NALPHA = 6.0, ALSCHD(1) = -5.0, 0.0, 5.0, 10.0, 15.0, 20.0,
NALT = 3.0, ALT(1) = 0.0, 5000.0, 10000.0, WT = 2300.0, LOOP = 3.0$
PLOT
SAVE
CASEID MACH 3.5
$FLTCON NMACH = 1.0, MACH(1) = 3.5,
NALPHA = 6.0, ALSCHD(1) = -5.0, 0.0, 5.0, 10.0, 15.0, 20.0,
NALT = 3.0, ALT(1) = 0.0, 5000.0, 10000.0, WT = 2300.0, LOOP = 3.0$
PLOT
SAVE
NEXT CASECASEID MACH 4.0
$FLTCON NMACH = 1.0, MACH(1) = 4.0,
NALPHA = 6.0, ALSCHD(1) = -5.0, 0.0, 5.0, 10.0, 15.0, 20.0,
NALT = 3.0, ALT(1) = 0.0, 5000.0, 10000.0, WT = 2300.0, LOOP = 3.0$
PLOT
SAVE