Two Jet Performance Spreadsheet
Summary: Max vertical takeoff weight 4800 pounds, 420 MPH initial cruise, 1000 pounds people and baggage, 1400 pounds maximum fuel, 2500 mile range with reserve at 45,000 feet.
Input Variables and Assumptions:
| 125 |
AREA WING DRAG; Root Chord = 45", Tip Chord = 30" |
| 125 |
AREA WING LIFT |
| 18 |
AREA HORIZONTAL STAB |
| 32 |
AREA VERTICAL STAB |
| 220 |
FUSELAGE WETTED AREA |
| 10 |
MAST WETTED AREA |
| 60 |
BOOM WETTED AREA |
| 10 |
SPINNER WETTED AREA |
| 0.007 |
COEFF DRAG AIRFOIL |
| 0.0035 |
COEFF DRAG WETTED |
| 0.2 |
WING INTERFERENCE DRAG - FLAT PLATE EQUIV. - SQ.FT. |
| 0.2 |
JET NACELLE INTERFER DRAG - FLAT PLATE EQUIV. - SQ.FT. |
| 0.2 |
FUSE & PYLON INTERF DRAG - FLAT PLATE EQUIV. - SQ.FT. |
| 0.1 |
TAIL INTERFERENCE DRAG - FLAT PLATE EQUIV. - SQ.FT. |
| 0.95 |
WING EFF |
| 40 |
SPAN - FT. |
| 40 |
ROTOR DIA. - FT. |
| 40 |
AREA OF BLADE |
| 80 |
RPM - ROTOR |
| 2 |
NUMBER OF ENGINES |
| 0.7 |
SPEC FUEL CONS- # FUEL / HR / # THRUST |
| 100 |
PERCENT OF MAX CRUISE THRUST |
| 4800 |
WEIGHT GROSS |
| 3400 |
WEIGHT LANDING W/O FUEL |
Calculated Results:
| ALTITUDE |
0 |
15 |
30 |
40 |
45 |
50 |
| RHO |
0.00238 |
0.0015 |
0.000889 |
0.000582 |
0.000459 |
0.000361 |
| V SOUND FPS |
1116 |
1057 |
995 |
972 |
972 |
972 |
| VEL FPS |
473 |
523 |
581 |
617 |
620 |
582 |
| VEL MPH |
322 |
356 |
396 |
420 |
422 |
396 |
| CL WING |
0.14 |
0.19 |
0.26 |
0.35 |
0.44 |
0.63 |
| PROFILE HP |
681 |
581 |
473 |
369 |
296 |
193 |
| INDUCED HP |
16 |
22 |
34 |
49 |
62 |
83 |
| ROTOR HP |
71 |
60 |
49 |
38 |
31 |
20 |
| TOTAL HP |
767 |
664 |
556 |
457 |
388 |
296 |
| DRAG-THRUST |
892 |
698 |
526 |
407 |
344 |
280 |
| MPG |
3.19 |
4.52 |
6.66 |
9.13 |
10.85 |
12.54 |
| L/D |
5.38 |
6.88 |
9.13 |
11.79 |
13.94 |
17.15 |
| BSFC - EQUIV. |
0.81 |
0.74 |
0.66 |
0.62 |
0.62 |
0.66 |
| RANGE |
854 |
1209 |
1783 |
2454 |
2903 |
3355 |
| TIP SPD ADV FPS |
640 |
691 |
749 |
784 |
787 |
750 |
| REY/FT. |
3009077 |
2270657 |
1639190 |
1738862 |
986023 |
741095 |
Fixed Calculations:
| 12.80 |
|
ASPECT RATIO |
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| 2.98 |
|
FLAT PLATE EQ. AREA W/O ROTOR |
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|
| 0.31 |
|
FLAT PLATE EQ. AREA ROTOR |
|
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| 3.29 |
|
TOTAL FLAT PLAT EQ. AREA |
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| 1257 |
|
ROTOR SWEPT AREA |
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| 168 |
|
ROTOR TIP SPEED - FPS |
|
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| 3.82 |
|
ROTOR DISK LOADING #/sq. ft. |
|
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| 38.40 |
|
WING LOADING #/sq. ft. |
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