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

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CONTENTS SUMMARY 1 INTRODUCTION SYMBOLS TECHNOLOGY IDENTIFICATION Propeller Performance Generalization Static and Forward Flight Reverse Propeller Noise Generalization Propeller Weight Generalization Propeller Cost Generalization Computer Program PARAMETRIC STUDY OPTIONS COMPUTER PROGRAM USAGE INSTRUCTIONS Program Input Program Output Messages Sample Cases CONCLUDING REMARKS REFERENCES TABLES I Advanced General Aviation Propeller Study - Aircraft Classification II General Aviation - Generalized Propeller Weight Equation FIGURES 1 Power Coefficient Chart for a 2-Bladed, 150 Activity Factor, 0.500 Integrated Design C L. Propeller 1 3 5 7 7 7 9 11 13 13 14 17 17 18 21 23 24 26 26 27 28 29
FIGURES (Contined) 2 3 4 5 6 7 8 9 10 11 12 13 14 IA 2A 3A APPENDIX CONTENTS (Contents) Thrust Coefficient Chart for a 2-Bladed 150 Activity Factor, 0.500 Integrated Design C Propeller Li Basic Performance Curve-Variation of Effective Torque Coefficient with Advance Ratio and Blade Angle. Basic Performance Curve-Variation of Effective Thrust Coefficient with Advance Ratio and Blade Cycle Basic Noise Curve. Category I Parametric Study Category 11 Parametric Study Category IV Parametric Study Example Reverse Thrust Variation with Landing Speed and Power Setting Sample Input Coding Sample Output - SHP Option Sample Output - Thrust Option Sample Output - 50% Stall Option Sample Output - Reverse Thrust Option Computer Program Flow Chart List of Subroutines FORTRAN IV Listing A Flow Charts, Subroutine List, and FORTRAN IV Listing for Hamilton Deck H432 Standard 45 vi 30 31 32 33 34 35 36 37 38 40 41 42 43 46 47 48
Page 1 and 2: k .” c - 1. -a “ ”- NASA *o *
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 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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