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

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Propeller 1. Diameter range 2. Number of blades range (2-8) 3. AF range (80-200) 4. C range (0.3 - 0.8) Li Operating conditions (maximum of 10). - For static and forward flight computation options, the following is required. 1. Shaft horsepower or thrust 2. Altitude, ft. 3. Velocity, knots 4. Temperature, OF 5. Tipspeed range For the reverse flight computational option, the following is required. 1. Normal rated take-off horsepower, SHP 2. Normal rated take-off speed, rpm 3. Altitude, ft. 4. Touchdown speed, knots 5. Temperature, OF 6. Range of power settings, % of normal rated shaft horsepower 7. Type of engine, reciprocating or turbine - Other 1. Number of engines 2. Distance from the propeller center of the desired field point at which the noise is to be measured. 15
3. Airplane classification (Table I) 4. Flight design Mach number 5. Performance computation options 6. Cost computation options The pertinent input-output instructions are discussed later in the text. 16
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 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 and 58: FORTRAN I V G LEVEL 20.1 MA IN OATE
Page 59 and 60: FClQTR41 IV G LEVEL 70.1 INPUT DATE
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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