XV-15 litho - NASA's History Office

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182 Tischler, M. B.; Leung, J. G. M.; Dugan, D. C. “Frequency-Domain Identification of XV-15 Tiltrotor Aircraft Dynamics in Hovering Flight.” Journal of the American Helicopter Society, April 1985. Tischler, M. B.; Leung, J. G. M.; Dugan, D. C. “Identification and Verification of Frequency-Domain Models for XV-15 Tilt-Rotor Aircraft Dynamics.” NASA TM-86009, 1984. Tischler, M. B.; Leung, J. G. M.; Dugan, D. C. “Identification and Verification of Frequency-Domain Models for XV-15 Tiltrotor Aircraft Dynamics in Cruising Flight.” Journal of Aircraft, vol. 9, No. 4, July-August 1986. Tischler, Mark B. “Advancements in Frequency-Domain Methods for Rotorcraft System Identification.” Vertica, vol. 13, no. 3, 1989. Tischler, Mark B.; Kaletka, Juergen. “Modeling XV-15 Tilt-Rotor Aircraft Dynamics by Frequency and Time-Domain Identification Techniques.” AGARD, Rotorcraft Design for Operations, 1987. Totah, Joseph J.; Madden, John F., III. “Rotor and Control System Loads Analysis of the XV-15 With the Advanced Technology Blades.” Innovations in Rotorcraft Test Technology for the 90s. Proceedings of the AHS National Technical Specialists’ Meeting, Scottsdale, Arizona, October 8–12, 1990. Totah, Joseph J.; Madden, John F., III. “Rotor and Control System Loads Analysis of the XV-15 With the Advanced Technology Blades.” NASA TM- 102876, 1991. Unger, G. “Tilt Rotor Aircraft and the U.S. Navy.” Fourth European Rotorcraft and Powered Lift Aircraft Forum, Italy, September 1978. VanWagensveld, D.; Magee, J. P.; et al. “Wind Tunnel Test of the Aerodynamics and Dynamics of Rotor Spin Up and Stopping and Folding a Semispan Folding Tilt Rotor Model.” AFFDL-TR-71-62, vol. VIII, October 1971. Weiberg, J. A.; Dugan, D. C.; Gerdes, R. “XV-15 N703 Takeoff Performance.” NASA Ames Memo dated January 4, 1983. Weiberg, J. A.; Dugan, D. C.; Gerdes, R.; Tucker, G. “Climb Performance of N703.” NASA Ames Memo dated April 7, 1983. Weiberg, J. A.; Maisel, M. D. “Wind-Tunnel Tests of the XV-15 Tilt Rotor Aircraft.” NASA TM-81177 and AVRADCOM TR-80-A-3,April 1980. Wellman, Brent. “Advanced Technology Blade Testing on the XV-15 Tilt Rotor Research Aircraft.” AHS 48th Annual Forum, Washington, D.C., June 3-5, 1992.
Wernicke, K. G. “Performance and Safety Aspects of the XV-15 Tilt Rotor Research Aircraft.” Presented at the 33rd Annual National Forum of the AHS, Washington, D.C., AHS Paper No. 77.33-14, May 1977. Wernicke, K. G. “Tilt Proprotor Composite Aircraft, Design State of the Art.” Journal of the American Helicopter Society, vol. 14, no. 2, April 1969, pp. 10–25. Wernicke, K. G. “Tilt-Proprotor Composite Aircraft, Design State of the Art.” Presented at the 24th Annual Forum of the AHS, Washington, D.C., May 8-10, 1968. Wernicke, K. G.; Edenborough, H. K. “Full Scale Proprotor Development.” Preprint No. 501, 27th Annual National V/STOL Forum of the AHS, Washington, D.C., May 1971. Wernicke, K. G.; Magee, J. P. “XV-15 Flight Test Result Compared with Design Goals.” Presented at AIAA Aircraft Systems and Technology Meeting, New York, New York, AIAA Paper 79-1839, August 1979. Wernicke, Kenneth G. “Mission Potential of Derivatives of the XV-15 Tilt Rotor Research Aircraft.” AGARD Paper No. 19, Paris, France, April 6-9, 1981. Wernicke, Kenneth G.; Edenborough, H. Kipling. “Full-scale Proprotor Development.” Journal of the American Helicopter Society, vol. 17, no. 1, January 1970, pp. 31–40. Wernicke, R. K. “A Tilt Rotor Design That Provides Economical Extended Range VTOL Transportation to Off-Shore Oil Platforms.” Presented at the AIAA Aircraft Systems and Technology Meeting, Anaheim, California, Paper No. 80- 1822, August 1980. Wernicke, R. K. “Prediction of Tilt Rotor Outwash.” Presented at the AIAA 19th Aerospace Sciences Meeting, January 12-15, 1982, St. Louis, Missouri, AIAA Paper 81-0013, January 1981. Wernicke, R. K. “XV-15 Tilt Rotor Aircraft and Preliminary Design of a Larger Aircraft for the U.S. Navy Subsonic V/STOL Mission.” Presented at the Fourth European Rotorcraft and Powered Lift Aircraft Forum, Stresa, Italy, Paper No. 45, September 1978. Wernicke, R. K.; Fischer, J. N. “An Evaluation of Advanced Rotorcraft Configurations for Emerging Military Applications.” Presented at the 37th Annual AHS Forum, New Orleans, Louisiana, May 1981. Wernicke, R. K.; Wernicke, K. G.; Borgman, D.C. “Mission Potential of Derivatives of the XV-15 Tilt Rotor Research Aircraft.” Presented at the 36th Annual Forum of the AHS, Washington, D.C., Paper No.80-11, May 1980. 183
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
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List of Figures Figure 1 Leonardo d
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Figure 41 Simultaneous static test
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Figure A-2 Transcendental Model 2 t
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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
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114 tiltrotor aircraft program. Thi
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116 Model 1-G Characteristics Power
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Figure A-3. Transcendental Model 2
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Figure A-4. XV-3 three-view drawing
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Figure A-5. XV-3 inboard drawing, s
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Nacelle angle (degrees) 124 120 90
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Figure A-8. General layout and majo
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Figure A-9. Side view inboard profi
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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 190 and 191: 164 Appendix F—Bibliography Tilt
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 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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