XV-15 litho - NASA's History Office

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164 Appendix F—Bibliography Tilt Rotor Related Publications Acree, C. W.; Jr. Tischler, M. B. “Using Frequency-Domain Methods to Identify XV-15 Aeroelastic Modes.” NASA TM-100033, November 1987. Acree, C. W., Jr. “An Improved CAMRAD Model for Aeroelastic Stability Analysis of the XV-15 With Advanced Technology Blades.” NASA TM-4448, 1993. Acree, C. W., Jr.; Tischler, M. B. “Identification of XV-15 Aeroelastic Modes Using Frequency Sweeps.” Journal of Aircraft, vol. 26 no. 7, July 1989, pp. 667-674. Acree, C. W., Jr.; Tischler, Mark B. “Determining XV-15 Aeroelastic Modes from Flight Data with Frequency-Domain Methods.” NASA TP-3330 and ATCOM Technical Report 93-A-004, 1993. Acree, C. W., Jr.; Tischler, Mark B. “Frequency-Domain Identification of Aeroelastic Modes.” NASA Tech Brief ARC-12407, 1991. Acree, Cecil W., Jr.; Tischler, Mark B. “Identification of XV-15 Aeroelastic Modes Using Frequency-Domain Methods.” NASA TM-101021, 1989. Ahuja, K. K. “Tilt Rotor Aircraft Noise: A Summary of the Presentations and Discussions at the 1991 FAA/Georgia Tech Workshop.” DOT/FAA/RD-91, 1992. Alexander H. R.; Amos, A. K.; Tarzanin, F. J.; Taylor, R. B. “V/STOL Dynamics and Aeroelastic Rotor-Airframe Technology.” AFFDL-TR-72-40, vol. 2, Boeing Vertol Co., September 1972. Alexander, H. R.; et al: “Preliminary Design Study of Advanced Composite Blade and Hub and Nonmechanical Control System.” NASA CR-152336, November 1979. Alexander, H. R.; Hengen, L. M.; Weiberg, J. A. “Aeroelastic Stability Characteristics of a V/STOL Tilt Rotor Aircraft with Hingeless Blades: Correlation of Analysis and Test.” AHS Preprint 835, Presented at AHS 30th National Forum, Washington, D.C., May 1974. Alexander, H. R.; Kuntz, W. H.; Wasserman, L. S. “Dynamically Similar Model Tests of Rotary Wing and Propeller Types of VTOL Aircraft.” U.S. Air Force V/STOL Technology and Planning Conference, Las Vegas, NV, September 1969. Alexander, Harold R.; Maisel, Martin D.; Giulianetti, Demo J. “The Development of Advanced Technology Blades for Tilt-Rotor Aircraft.” 11th European Rotorcraft Forum, London, England, September 10–13, 1985. Amos, A. K.; Alexander, H. R. “Simulation Study of Gust Alleviation in a Tilt Rotor Aircraft.” Vols. I and II, NASA CR-152050/1, June 1977.
Anon. Bell’s XV-3. AEROPHILE, vol. 2, no. 1, ISSN0147-7668, June. 1979. Anon. “Civil TiltRotor Development Advisory Committee Report to Congress in Accordance With PL102-581.” December 1995. Anon. “Civil TiltRotor Missions and Applications, Phase II: The Commercial Passenger Market.” NASA CR 177576, February 1991. Anon. “Full-Scale Hover Tests 25-Foot Low Disk Loading Tilt Rotor.” NASA CR-114626, May 1973. Anon. “Large Scale Wind Tunnel Investigation of a Folding Tilt Rotor.” NASA CR 114464, Bell Helicopter Co., May 1972. Anon. The XV-15, Bell’s Tilting Test Bed. AEROPHILE, vol. 2, no. 2, ISSN0147-7668, October 1979. Anon. V/STOL Tilt-Rotor Research Aircraft,Vols. 1–4. Bell Helicopter Co., Reports 301-199-001 to 004, 1975. Anon. “V/STOL Tilt-Rotor Aircraft Study, Vol. II—Preliminary Design of Research Aircraft.” NASA CR-114438, Boeing-Vertol Co., March 1972. Anon. “V/STOL Tilt-Rotor Study, Task II—Research Aircraft Design.” NASA CR-114442, Bell Helicopter Co., March 1972. Anon. “Wind Tunnel Results. Advancement of Proprotor Technology, Task II.” NASA CR-114363, Bell Helicopter Co., September 1971. Anon. “Wind Tunnel Test Results of 25-Foot Tilt Rotor during Autorotation.” NASA CR-137824, February 1976. Anon. “XV-15 Flight Manual.” Bell Helicopter Textron Report TP-78-XV-15-1, August 15, 1980. Arnold, James R.; Farrell, Michael K. “One Engine Inoperative Takeoff Climb Performance of the XV-15 Tilt Rotor.” SAE, Aerospace Technology Conference and Exposition, Long Beach, California, October 5–8, 1987. Arrington, W. L.; Kumpel, M.; Marr, R. L.; McEntire, K. G. “XV-15 Tilt Rotor Research Aircraft Flight Test Report.” Vol. I-V, NASA CR 177406 and USAAVSCOM TR-86-A-1, June 1985. Baird, Eugene F.; Bauer, Elmer M.; Kohn, Jerome S. “Model Tests and Analyses of Prop-Rotor Dynamics for Tilt-Rotor Aircraft.” Mideast Region Symposium of the AHS, Philadelphia, Pennsylvania, October 1972. 165
Page 1:
The History of The XV-15 Tilt Rotor
Page 5:
Contents Prologue . . . . . . . . .
Page 9:
Dedication The story of the success
Page 13:
Foreword The development of tilt ro
Page 17 and 18:
List of Figures Figure 1 Leonardo d
Page 19 and 20:
Figure 41 Simultaneous static test
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Figure A-2 Transcendental Model 2 t
Page 23 and 24:
List of Acronyms AARL Army Aeronaut
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TRENDS Tilt Rotor Engineering Datab
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Figure 2. Illustration of vertical
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Figure 4. McDonnell XV-1 compound h
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Figure 7. Henry Berliner tiltpropel
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Top: Figure 9. The Baynes Heliplane
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Figure 13. Illustration from the Ha
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Figure 17. Bob Lichten, extreme lef
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Figure 20. Tiedown tests of the XV-
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16 Research and Engineering), obtai
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18 management continued to show int
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20 Building the Technology Base Aer
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Figure 25. Bell 25-ft. diameter pro
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Figure 28. Performance tests of 5-f
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Figure 31. Bell 25-ft. diameter pro
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28 Tilt Rotor Research Aircraft Pro
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30 During the late 1960s and early
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32 range of loading conditions and
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34 The initial projected cost of $4
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Figure 35. Illustration of the Boei
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Figure 36. 1/5 scale XV-15 model in
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40 under the contract. To accomplis
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42 Aircraft Development The primary
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44 Test stand angle box Test stand
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Figure 40. Proprotor response to co
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Figure 41. Simultaneous static test
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50 helicopters. For the conversion
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52 Prior to the start of flight ope
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Figure 44. Initial Bell tiedown sho
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56 degrees 25 and a brief assessmen
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Figure 45. XV-15 in the Ames Resear
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60 NAVAIR managers as a means of de
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Figure 46. Government and Bell pers
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Figure 49. Tiedown test facility at
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66 Wheel height Top: Figure 51. Met
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68 Symmetric beam mode Antisymmetri
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Figure 55. XV-15 during short takeo
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Top: Figure 56. Flow visualization
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74 during “degraded” flight con
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Figure 59. Hover acoustics tests du
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78 Nose weight Top: Figure 61. Typi
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80 Following the completion of cont
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82 After the proprotors stopped, th
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84 sudden stoppage of the right eng
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86 A reconversion to the helicopter
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88 Paris Air Show By early 1981, th
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90 enroute from Farnborough to Fran
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Top: Figure 66. Senator Goldwater i
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Figure 69. Shipboard evaluations of
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Figure 71. XV-15 at the New York Po
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98 Crash (October 16 and 17, 1991).
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100 The End of an Era By the mid 19
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Top: Figure 73. XV-15 at the Dallas
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104 management system was very effe
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106 could make use of the same flig
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Figure 76. The Bell tilt rotor eagl
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110 demonstrations two years earlie
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112 Future Tilt Rotor Aircraft By t
Page 140 and 141: 114 tiltrotor aircraft program. Thi
Page 142 and 143: 116 Model 1-G Characteristics Power
Page 144 and 145: Figure A-3. Transcendental Model 2
Page 146 and 147: Figure A-4. XV-3 three-view drawing
Page 148 and 149: Figure A-5. XV-3 inboard drawing, s
Page 150 and 151: Nacelle angle (degrees) 124 120 90
Page 152 and 153: Figure A-8. General layout and majo
Page 154 and 155: Figure A-9. Side view inboard profi
Page 156 and 157: Figure A-11. XV-15 height-velocity
Page 158 and 159: 132 Weight Design . . . . . . . . .
Page 160 and 161: 134 WBS LEVEL: Bell Army/NASA I II
Page 162 and 163: 136 US Army Air Mobility Research a
Page 164 and 165: 138 Army/NASA (continued) Staff (19
Page 166 and 167: 140 Appendix C—Chronology 1452-15
Page 168 and 169: 142 1968 Boeing Vertol awarded cont
Page 170 and 171: 144 November, Initial piloted simul
Page 172 and 173: 146 24 March 1982 XV-15 demonstrate
Page 174 and 175: 148 30 July 1987 FAA/NASA/DOD Tilt
Page 176 and 177: 150 21 August 1990 V-22 reached 340
Page 178 and 179: 152 14 June 1993 The Department of
Page 180 and 181: 154 Appendix D—Awards and Records
Page 182 and 183: Figure D-1. Jean Tinsley, first wom
Page 184 and 185: Figure E-3. XV-15 flying by the Sta
Page 186 and 187: Figure E-7. Bell test pilots Roy Ho
Page 188 and 189: Figure E-11. Ken Wernicke, Bell til
Page 192 and 193: 166 Ball, J. C. “XV-15 Shipboard
Page 194 and 195: 168 Churchill, G. B.; Dugan, D. C.
Page 196 and 197: 170 Edenborough, H. K. “Investiga
Page 198 and 199: 172 Harendra, P. B.; Joglekar, M. J
Page 200 and 201: 174 Kvaternik, Raymond G. “Studie
Page 202 and 203: 176 Magee, J. P.; Pruyn, R. “Pred
Page 204 and 205: 178 Martin, Stanley, Jr.; Erb, Lee
Page 206 and 207: 180 Rutledge, Charles K.; George, A
Page 208 and 209: 182 Tischler, M. B.; Leung, J. G. M
Page 210 and 211: 184 Whitaker, H. L.; Cheng, Yi. “
Page 212 and 213: 186 Daniel C. Dugan Daniel Dugan gr
Page 214 and 215: 188 Carnet, 88 Carpenter, Ron, 91 C
Page 216 and 217: 190 Moffett Airfield, Moffett Field
Page 219 and 220: Monographs in Aerospace History Lau
Page 222: National Aeronautics and Space Admi
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