COMPUTER PROGRAM USER'S MANUAL FOR ... - CAFE Foundation
COMPUTER PROGRAM USER'S MANUAL FOR ... - CAFE Foundation
COMPUTER PROGRAM USER'S MANUAL FOR ... - CAFE Foundation
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HAMILTON SlANDARD <strong>COMPUTER</strong> DECK NO. H432<br />
COMPUTES PER<strong>FOR</strong>HANCEINOISE~WEIGHT~ANO COST <strong>FOR</strong><br />
GENERAL AVIATION PROPELLERS<br />
1 AIRPLANE IN CATEGORY 1V SAMPLE CASE 3<br />
2 SHP INPUT-CALC. TIPSPEED <strong>FOR</strong> 50PERCENT STALL-COST <strong>FOR</strong> RANGE QUANT.<br />
OPERATING CONOITION<br />
SHP<br />
ALT-FT<br />
=<br />
=<br />
740.<br />
0.<br />
NO. OF ENGINES = 2.<br />
DESIGN FLIGHT M.=0.327<br />
UNIT FACTOR L.C.<br />
1000 FACTOR L.C.<br />
= 3.22<br />
= 1.02<br />
V-KTAS = 77.5 CLISSIFICATION = 4.<br />
TEMP R = 519. FIELO POINT FT. = 500.<br />
NUMBER BLAOES= OF 4. ACTIVITY FACTOR-200. INTEGRATED DES1G.N CL =.600<br />
*** 1970 TFCHNOLOGY *** *** 1980 TECHNOLOGY ***<br />
0IA.FT. T.S.FPS THRUST PNL QUANTITY WT-LBS SCOST QUANTITY UT-LBS SCOST ANGLE FT M J CP CT. -<br />
a. 345. BLR. 77. 1. 228. 7106. 1. 185. 7770. 46.3 1.000 0.1172 1.194 0.9333 0.4473<br />
1001. 228. 2252. 1001. 1a5. 2463.<br />
2001. 228. 2~07. 2001. 185. 2195.<br />
3001. 22a. 1876. 3001. 185. 2052.<br />
4001. 228. 1788. 4001. 185. 1956.<br />
NUMBFR OF BLADES= 6. ACTIVITY FACTOR=200. INTEGRATED DESIGN CL =.600<br />
*** 1970 TECHNOLOGY *a* *** 1980 TECHNOLOGY ***<br />
DIA.FT. T.S.FPS THRUST PNL QUANTITY WT-LBS SCOST QUANTITY UT-LBS SCOST ANGLE FT M J CP CT<br />
8. 282. 828. 74. 1. 306. 11926. 1. 245. 12887.<br />
1001. 306. 3780. 1001. 245. 4084.<br />
2001. 306. 3368. 2001. 245. 3640.<br />
3001. 306. 3149. 3001. 245. 3403.<br />
4001. 306. 3002. 4001. 245. 3244.<br />
FIGURE 13. SAMPLE OPTION - 50% STALL OPTION<br />
51.2 1.000 0.1171 1.459 1.7021 0.6759