LOW REYNOLDS NUMBER VEHICLES - FTP Directory Listing - NATO

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NORTH ATLANTIC TREATY ORGANIZATION ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT (ORGANISATION DU TRAITE DE L'ATLANTIQUE NORD) AGARDograph No.288 LOW REYNOLDS NUMBER VEHICLES by Thomas LMueller University of Notre Dame Notre Dame, Indiana 46556 USA Edited by Eli Reshotko Case Western Reserve University Cleveland, Ohio 44106 USA AGARD-AG-288 This AGARDograph has been produced at the request ofthe Fluid Dynamics Panel of AGARD.
Page 1: 001 00
Page 5 and 6: ACKNOWLEDGEMENTS It is a pleasure t
Page 7 and 8: SUMMARY LOW REYNOLDS NUMBER VEHICLE
Page 9 and 10: As a result of this critical bounda
Page 11 and 12: oundary layer equations 36 ' 71 . R
Page 13 and 14: 3.1 The Eppler Airfoil Design and A
Page 15 and 16: "viscous-lnviscid" procedure. Refer
Page 17 and 18: Also, PrVrL • Ur rmg r 'W TP - CP
Page 19 and 20: A fixed static and total pressure r
Page 21 and 22: The EPPLER 61 airfoil has been stud
Page 23 and 24: There was a noticeable increase in
Page 25 and 26: In earlier experiments by Conigllar
Page 27 and 28: In the course of these studies, the
Page 29 and 30: 5.1 Remotely Piloted Vehicles and S
Page 31 and 32: REFERENCES 4) To improve the experi
Page 33 and 34: 45. Schmitz, F.W., "Aerodynamics of
Page 35 and 36: 95. Doligalskl, T.L., Smith, C.R.,
Page 37 and 38: 147. Payne, F.M., and Nelson, R.C.,
Page 39 and 40: Csl E CO IO- 10 10 < 10 UJ tT < -2
Page 41 and 42: HIGHCW or t-1 CLOCKWISE HYSTERESIS
Page 43 and 44: Figure 16, Flow About an NACA 23012
Page 45 and 46: Cj Cf THEORY -— EXPERIMENT (ref.
Page 47 and 48: Figure 23. Plot of Computed Streaml
Page 49 and 50: LEADING EDGE Figure 29. Smoke-Wire
Page 51 and 52: a) NACA 663-OI8 b) EPPLER 61 NACA 6
Page 53 and 54:
•LISSAMAN •MILEY Figure 40. Lis
Page 55 and 56:
SOUND PRESSURE LEVEL ONE FLOW RESTR
Page 57 and 58:
a) Increasing Angle of Attack b) De
Page 59 and 60:
MILEY Rc= 150,000 I H 6 T 12 •- 0
Page 61 and 62:
a (J - -4 n -3 u. UJ O a a: D IN -
Page 63 and 64:
Wortmonn FX 53-137 Corrected dot Rc
Page 65 and 66:
Wortmann FX 63-137 Corrected data R
Page 67 and 68:
Wortmann FX 63-137 Uncorrected data
Page 69 and 70:
180 170 160 1.50 140 1,30 120 110 o
Page 71 and 72:
1,8 1.6 o" 1.4 ^ 12c-.., o o 1.0 ^
Page 73 and 74:
a) Horizontal Axis Propeller-Type b
Page 75 and 76:
0.5 THRUST COEFFICIENT (C,)
Page 77 and 78:
X K ri d v JB • E M C < a C y a I
Page 80:
£_M£mmlm NATO ^ OTAN 7 RUE ANCELL
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