模型飛行機による飛行中の空力データ測定と 失速特性の解析について
Contents
1. 2 8 1 17 3 3 3 1 32. 119 sec 4 28 9 7 4 29 Cp 0 5 0 5 38
3. 2 8 U CAN FLY 2 1 0 865m2 1 67kg 11 1V 2200mAh Li Po INACA2415 2 1 2 2 2 2 2 EPO ASTRO HOBBY Cessna 310 Grand Cruiser
4. GOPRO HERO3 170 HD 100g 12 2 15 iON the Action 2 16 GOPRO HERO3 13 2 3 2 3 1 2500 SONY HDR 2000AX Ne
5. 4 3 1 3 30 0 419 4 3 1 2 4 69 60 4 70 4 71 61 4 72 4 73 62 mys aldeg 13LU sec 4 74 150 151 al see 4 75 4 70 4 59 V 7 1m s o 20
6. 4 76 STOL 4 3 2 C 2 CZ 1 2 x z az az 64 ms a Cosa 4 77 L ma COSC 4 5 L poV SC 4 6 2 a 47 pyV 9 poV Scosa az a Cz
7. CFD
8. CL thired1 CL hr 1 CL r 0 CL ah cn IiHeg 4 79 30 1 6 MI 2 4 1G 0 8 1G
9. 2 1 2
10. 8 300mm 270mm 1 4 2 1 1 28 4 11 4 12 29 4 18 4 14 30 4 15 Cp 0 12345678 5 0 hi T 4 16 T Osec T 70sec T 120sec T 170sec T 280sec 4 2 1 Cp 8 8
11. 2 5 10 gt gt gt
12. 2 17 2500 14 2 18 HDR 2000AX 2 3 2 5 2 19 COSMO DAQ PC 15 _ 3 3 1 3 1 1 90m 3 1 16 3 2 3 1 2
13. 19 3 7 Google Earth 3 8 20 3 2 3 2 1 0 3 3V ADC 10bit 100Hz 3 1 3 3 3 2 1024 Data A FE a 11 111 DSS 1 1 Ideal 1 Tatal Errer Band 0 1 2 3 4 EE 7 B 8 10 F Pa Pressure inH20 Output VV SPY x Pressure ea Prin 0 10 x Vsupply a 3 9 0 HSC Series ULP Analog PS zzz Vp Pressureappzeg
14. Micro SD PC 3 4 18 3 5 8 6 1 2
15. 17 22 30 a 4 zz AC AO 4 1 7 max 7 4 Crmazjbase 7 TDNET HI LDL LT FPPELL2 1 1 1 TT et Tt 2 2 1 TTP LLTT 1 HT 10 12 14 6 1 30 20 20 28 33 oT PLAPCHORD wing chord n 1 1
16. GPS 10 2 12 GPS GT 730FL S 2 13 ArduPilotMega 2 5 2 2 3 3 11 FLY DV 1ON The Action e GOPRO HERO8 FLY DV 1 PC 2 14 FLY DV 10N the Action 2 FLY DV 60
17. D Cp Cp 31 Cp 1 dj tf 1 ne Tep DD Fh ted 15dep Wr dtline S nD 1 1 0 s DB 1 JE 4 17 Cp 15 Cp PE 3 HL1 tf J 1 nn liniep 3 mh igh ru ke i a LIMP re nD 1 j 1 3 0 5 li 8 1 w e 4 18 Cp 10 Cp BB 1 Ff 1 El 5 iF Fi FT TH i Mn Cum Ti 1 1 1 3 5 6 DB 1 4 19 Cp 5 Flight test Cp Wind tunnel Cp
18. yaw diff_pitch 4 4 DO D 2 5 Pitch 0 0493 1 deg Yaw 0 0490 1 deg 702 4 1 2 5 5 5 5 5 100mm 26 4 5 5 100mm 3 pha Alpha artual inffmm 1 15 1 EE 0 2 eg dag _ 1 4 6 100mm 5m s 3 TT hl nha mw lha srtual inffm
19. 5 gt 10 20 1G 66 4 78
20. CFD 1 2 1 1 5 G
21. 0 059 1 deg 2 D NACA2415 e 0 096 1 deg 0 62 1 8 88 2 3 0 72 4 85 KMAP 0 059 1 deg 0 069 17 deg ga 1 2 19 Cmax 2 2 8 A 5 88 19
22. 44 2008 10 IRAH ABBOTT ALBERT E VON DOENHOFF and LOUIS S STIVERS Jr SUMMARY OF AIRFOIL DATA REPORT No 824 NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS 1945 11 UAV MAV 72 721 2006 1 2 Honeywell Sensing and Control TruStability Board Mount Pressure Sensors HSC Semies High Accuracy 2012 1 3 Vladimir Brusov Jozef Grzybowski and Vladimir Petruchik Eight Data Acqguisition System for Small Unmanned Aerial Vehicles Proceedings of the International Micro Alr Vehicles conference 2011 69 1 4 M Serdar Genc Ilyas Karasu H HakanAcikel and M Tu grul Akpolat Low Reynolds Number Flows and Transition InTech 2012 1 5 MachineTalker Inc MachineTalker NASA UAV Board Hinal Report UAV Sensor Flight Test 2005 1 6 Fong Ming Yang Eugene UAV Flight Test System National University of Singapore 2008 17 Austin M Murch University of Minnesota UAV Flight Research Facility University of Minnesota AEM Department Seminar 2012 1 8 Sia Long Qiang Unmanned Aerial Vehicle UAV Flight Test System National University of Singapore 2012 19
23. gt oc L upper Pwer dX 1 c L PoY CD Cpiower dX 40 1 2 poV gt Cp gt Cp Ar 4 Ax Ax C gt Cp upper Cp lower C C 4 33 4 34 C1 41 2 NAOCA2415 Re 8 0X105 0
24. Vol 50 No 576 2002 2 0 2013 RC 70
25. 2 1 GPS 2 2 1 1 2 1 2 2 1 1 1 1 1
26. 2 4 ASTRO HOBBY Cessna 310 5 2 5 ASTRO HOBBY Cessna310 2 6 30 11 1V 2200mAh Li Po 2 NACA2418 NACA2412 7 30 5096 2 2 2 2 1 RN
27. gt gt 1 2 0 8 1 KMAP 2009 2 2009 68 3 1989 4 2005 5 W J McCroskey and 8 L Pucci Viscous Inviscid Interaction on Oscillating Airfoils in Subsonic Flow AIAA JOURNATL VOL 20 NO 2 FEBRUARY 1982 6 Sung Hyun Kim et al Calibration of a Hive Hole Multi Function Probe for Helicopter Air Data Sensors Int1 J of Aeronautical amp Space Seiences Vol 10 No 2 INovember 2009 7 M Serdar Genca Ilyas Karasu H Hakan Acikel An experimental study on aerodynamics of NACA2415 aerofoil at low Re numbers Experumental Thermal and Fluid Sclence 39 2012 8 gt 24 6 9
28. 2 0X105 4 26 36 4 27 a hb 4 27 a b 1 2 0 8
29. EPP EPO 1 5m TU CAN FLY 1400 PIP EPO JR PROPO DMSS 2 4GHz 5 8 XG8 RG831 2 1 UCAN FLY 2 2 XG8 RG831B 5 LM
30. 30 0 41 48 4 3 1 1 4 51 49 4 53 50 4 54 51 4 55 VIm tildeg sec 4 56 sec 4 57 4 52 V 9 8m s a 15deg 52
31. 0 75 2 42 WI Cin 2 NACAZ41S 15 4 36 Cl Fig 12 Unsteady airloads for cmse 7 NACA 012 airfoil x lO 5 sana 4 37 CL CM Viscous Inviscid Interaction on Oscillating Airfoils in Subsonic Flow e 0 5 1 0 o 2 k0 05
32. 1G 67 nis 5 5 3 2 3
33. 4 53 4 3 1 2 30 a 4 58 93 4 59 4 60 54 4 61 4 62 4 63 100 101 1 1 104 105 sec 4 64 56 1 101 1 02 to sl sec 4 65 80 4 59 V 8 5m s c 16deg 1 4 60
34. 1 5 75 8 16 2 5 959 10 20 2 75 85 95 5 2 2 2 GPS 1 2 GPS GPS ArduPilotMega2 5
35. NI 65 CL ap don CL Ep up NACAS415 Chr fap up 1H da 4 78 30 30 5 2 NACA2415 2 38380 0 3 1 2 8 2 3 NACA2415
36. es Tr i ee ie rr i mn a wi a Mai ml i i Ll mL EE a i i ny lt we jl We TI Ce py Be V 4 49 XYZ mm 4 50 15 T 15sece 2 T 110sec 30 T 125sec T 150sec T 170sec 3 T 215sec 2 ArduPilotMega2 5 GPS IMU 1 10 8 4 3 1 2 2 0
37. Pax MK ip J Output Vn x0 10 sup ply 3 3 a Vsupply 3 3V Pmax 21nH20 498 35Pa Prin 498 835Pa 9 Data Fied fin 99 1024 Ve x0 10 i supply 2 Data ee Rs A NT 8 4 5 2 8 g P lied a CPP ma Ly A w Ez aLE1 Ps f A Li ES 8 10 5 Calibration of a Five Hole Multi Function Probe for Helicopter Air Data Sensors
38. sec 4 30 4 81 Cp 39 4 32 4 2 3 CO 4 4 1 2 2 poV UL V D TT
39. PC csy Excel Google Earth Ba Fe 4 Lj 4 a 8 11 Mission Planner 23 3 12 Google Earth 4 4 1 5 4 1 1 5 5 5 10m s 4 1 5 24 25 stati Ps P ii deg 5 Pi tape Me 4 3 5
40. ES ee 3 3V 8 2 Micro SD 10 1 mi LE 3 2 7 2 8 a 2 i Honeywell HSCDRRNOO2NDAA3 Logomatic v2 Serial SD Datalogger 7 4V 180mAh Li Po 83 3V 2 8 5 2 10 1 2 11 2 5 1 2 1 1 2 2 5 15 25 5 10
41. 2 EOD 2 PPFaPi Pr P APs dP dP 2 3 5 2 q KgxP lt 3 6 Kg 1 96 9 oe 3 7 22 CD dP dP Cppicn gt 3 8 dP dP 2 a Kpx Cp pi 3 9 Kp 10 246 Cp P P C1 3 10 q 5 Cp 3 2 2 GPS GPS ArduPilotMega2 5 GPS PWM
42. 5 10 15 32 4 2 2 0 VIm s nlde 4 20 4 21 33 4 22 4 23 34 4 24 73 13 5 sec 4 25 35
43. Cs 4 43 4 3 2 2 gk 4 38 4 39 44 4 40 4441 45 4 43 46 4 44 4 47 47 a I W TH Li 1 Tb de Pm 1 1 Her ms bo WMLM LIM IALUA_ JI MT LIL Ji ui hw FT Lon ID UP yy a dh 9 i i i 1 EL Bi Pe 1 i mr Fe IT J Li 4 48 Cb ae i
44. SCL lin 4 66 kL k2k3 A Clnaibase KMAP 1506 32 30 kk3 1 4 Cmax base 1 6 k1 1 05 k2 0 88 A Cmax 1 48 Lmax 7 max lt 4 2 Or 8Swr 58 4 67 Sw Swr KMAP 0 44 AC 0 65 W max 4 68 W L gt pV SC 4 3 2W 4 4 poV 9 L L Cr 0 CZpa 1 62 59 80 CLmax 1 93 4 az 0 82 12
45. 20183 ss 1 1 UO ND A 1 2 2 2 0 2 2 1 1 1 1 oo 2 2 12 2 OO 4 Gk 7 ET 7 9 2 2 GPS eas ea 10 9299 7 11 2 3 i 14 2 14 Rs 5 cc OJ a 15 8 01 16 oe 16 SR 16 2 17 eo 18 2 21 EN CC 21 0 2 23 4 i 24 a1 BILE dn 24 A TT LE OE OANA di 24 4 12 TE IGE hes Ta 26 I a Og 28 42 1 OpNN EO 31 422 33 Og 40 4 8 2 nt 44 I 48 4 3 2 Cz 64 2 Nh i 68 eo 70 1 1 1 CFD
46. deg 2 63 4 max Cima 1 93 2 77 4 0 84
47. m 10 ks 2 15 G 1 EE 0 2 2 deg HUFET 1 4 7 100mm 10m s 100mm 10 100mm 300mm 27 4 8 5 300mm deg mal Url Vm i PE deg lde 10 5 5 1a 15 20 23 4 9 300mm 5m s de m s ee Wms Vm Pe deg dee i 4 10 300mm 10m s
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