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Page 1: NASA Technical Memorandum 4448 An I
Page 5: SYMBOLS General ct/_ K qfn R thrust
Page 8 and 9: illustratingthatminimumstiffness is
Page 10 and 11: etweenabout260and395KTAS,whereas it
Page 12 and 13: mostinboardsegment isthebladecuff,4
Page 14 and 15: transmission case, reducingwarpingo
Page 17 and 18: APPENDIX A: THE CAMRAD MODEL OF THE
Page 19 and 20: RADIUS = 12.5, NBLADE= 3, SIGMA = 0
Page 21 and 22: TWISTI ' For MASS 0.325, 0.400, 0.5
Page 23 and 24: IXY = 0., TRATIO = 1.0, ASHAFT = 2"
Page 25 and 26: FETAIL = 2016., LHTAIL = 22.0, HVTA
Page 27 and 28: _00_0______0_0_0_0_0__0 00000_____0
Page 29 and 30: 0_0000_ 0_0__ 0___ ,°,.°0o,°0 _0
Page 32 and 33: __0_ __0000 o.i,,,,o _000000 ___0_0
Page 35: 00______0_0_0_0_0_0_0 _0_00_00_____
Page 38 and 39: o 0_ d v (D _D 32 o 0_00_0_0_0_0_0_
Page 43 and 44: APPENDIX B: XV-15 CONTROL-SYSTEM ST
Page 45 and 46: Table 1. ATB configurations flown t
Page 47 and 48: Polyurethane erosion cap Clamp Fibe
Page 49 and 50: O "O "O t'- e-i x > en Q. C .w E O
Page 51 and 52: _" 6-t_ 0 "_ s-- "0 r- 0_ Q. > 4 ==
Page 53 and 54: i t_ "0 > t_ en t_ ,_= 4 m _E 1 Air
Page 55 and 56: Collective lever (walking beam) Col
Page 57 and 58: oo u) "0 > o e-, tf 05 (3- 05 r" t3
Page 59 and 60: Longitudinal cyclic Shim / / Inner

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