COMPUTER PROGRAM USER'S MANUAL FOR ... - CAFE Foundation

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FORTRAN I V G LEVEL 20.1 MAIN DATE = 72034 10/08/04 0238 0 239 0240 0241 0 242 0243 0244 0245 0246 0247 0248 0249 02 50 0251 0252 02 53 0254 0255 0256 02 57 0258 0259 0260 0261 0 262 0263 0264 0265 588' CON1 I NUE GO TO 40 730 GO TO (31r341rIW 31 WRITE16,32) OtA~lIPSPD,THRUSTIIC)tPNL,8LLLL~XFr,ZMl,ZJIrCP~CT 32 FOR~AT(F7.2rF7.O~F9.OIF6.OIF6.lrF8.31F7.4~F8~3t2F~~4~ GO TO 40 34 blRITE(6r32) DIA~TIPSPDrBHP~IClrPNLteLLLLL~XFT~Z~l~~JlrCP~CT 40 IFITRIG.EO.1.) GO TO 750 IF(ISTALL,EC. 2) GO TO 800 IFIIFIN.EQ.7710) GO TO 800 600 CONT I NUE IF (IW.LT.~) GO ro 750 C REVERSE THRUST CALCULATION 3000 IRl=NPCPW I I C 1 PCPWC=PCPW(ICI DO 3900 I=lrIRT IF (RTC-1.) 3200r3100~3200 3100 CP~BHPIIC~*PCPWC*ROROIIC)*10.E10/~2~O*R~~ClIC~*~3*DIA**5~lOO~~ 3200 CALL REVTHT ~RTCrROT,AFTrGL~~8LADT~DIA~CP,BETA(IC~,RUFOIIC~~ 1 BHP( I C 1 rRPMC(IC),PCPWCrANDVK(IC)) PCPWC=PCPWC+DPCPH I IC 1 3900 CONTINUE 750 COhTINUE 800 CONTINUE 1000 GONT I NUE LOO1 CONTINUE 1200 CONTINUE 700 CONT I NU€ GO TO 701 END FIGURE 3A. FORTRAN IV LISTING (CONTINUED) 53
FClQTR41 IV G LEVEL 70.1 INPUT DATE = 72031 , . , . , 08/48/14 FIGURE 3A. FORTRAN IV LISTING (CONTINUED) 54
Page 1 and 2:
k .” c - 1. -a “ ”- NASA *o *
Page 4 and 5:
CONTENTS SUMMARY 1 INTRODUCTION SYM
Page 6:
SUMMARY A major outcome of the stud
Page 10 and 11: AF b B C LD C Li cP C Q cT D h J M
Page 12 and 13: TECHNOLOGY IDENTIFICATION ' General
Page 14 and 15: cT T~~ - thrust coefficient - activ
Page 16 and 17: &AF - activity factor adjustment fa
Page 18 and 19: Propeller Weight Generalization A w
Page 20 and 21: Propeller 1. Diameter range 2. Numb
Page 22 and 23: PARAMETRIC STUDY OPTIONS Having dev
Page 24 and 25: 1. 2. 3. 4. 5. 6. 7. a. 9. 10. Card
Page 26 and 27: 6. RPM for zero velocity, full thro
Page 28 and 29: For the option where tipspeed for 5
Page 30 and 31: CONCLUDING REMARKS 1. Generalizatio
Page 32 and 33: j Aircraft Class Seats I. Single En
Page 34 and 35: Y (I) 4 w EFFECTIVE POWER COEFFICIE
Page 36 and 37: I 3 BLADES/IOO AF/O.~ cLi BLADE ANG
Page 38 and 39: PROPELLER INPUT HORSEPOWER FIGURE 5
Page 40 and 41: ~ ja, m ~ MINIMUM CRUISE 370# THRUS
Page 42 and 43: I CATEGORY V I LANDING SPEEDS, KNOT
Page 44 and 45: w W JOB NO.: ACCT. NO: W.O. NO.: !
Page 46 and 47: HAMILTON STANQARD CflMPUTER DECK Nf
Page 48: 2FClPR7CATIVG F'IGI'JF 650. 547. 21
Page 51 and 52: DETERMINE TIPSPEED AT WHICH BLADE W
Page 53 and 54: . FORTRAN .CY G LEVEL 2011 HA1 N DA
Page 55 and 56: FORTRAN .I.V G LEVEL 2011 . . MA I
Page 57: FORTRAN I V G LEVEL 20.1 MA IN OATE
Page 61 and 62: 0017 00 19 00 19 0020 0021 0022 56
Page 63 and 64: FORTRAN I V G LEVEL 20.1 PERFM DATE
Page 65 and 66: FORTRAN IV G LEVEL 20.1 PERFM DATE
Page 67 and 68: . " . -. . . . IDRTRAN .IV..G LEVEL
Page 69 and 70: FOPTRAU 1V C, LFVFL 23.1 ZNO I SF D
Page 71 and 72: FORTRAN I V G LEVEL.. 20.1 . . " .
Page 73 and 74: 0035 0006 0007 001 0 FIGURE 3A. FOR
Page 75 and 76: . .. F3RTpAN 1V.G LFVEL 20,l 0063 0
Page 77 and 78: FI?RTP.AY IV G LEVEL 20.1 R IOUAD D
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