XV-15 litho - NASA's History Office

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166 Ball, J. C. “XV-15 Shipboard Evaluation.” Presented at the AHS, 39th Annual Forum, St. Louis, Missouri, May 9–11, 1983. Ball, J. C.; Bowes, R. H. “Second Interim Report-USN/USMC Assessment of the XV-15 Tilt Rotor Research Aircraft.” NATC Report No. RW-29R-83, September 29, 1983. Ball, J. C.; DuFresne, D. A. “Shipboard Evaluation of the XV-15 Tilt Rotor Research Aircraft.” NATC Report No. RW-54R-82, April 18, 1983. Ball, John C. “Tilt-Rotor Memories.” Naval Helicopter Association Rotor Review, Number 19, November 1987. Bartie, K.; Alexander, H.; McVeigh, M.; Lamon, S.; Bishop, H. “Hover Performance Tests of Baseline Metal and Advanced Technology Blade (ATB) Rotor Systems for the XV-15 Tilt Rotor Aircraft.” NASA CR-177436, 1986. Becker, C. L.; Bowes, R. H.; Kolwey, S.; Clark, W. J. “Evaluation of the XV-15 Tilt Rotor Aircraft Concept for JVX Missions.” NATC Report No. RW-13R-85, May 12, 1986. Beroul, Frederic; Bassez, Pascal; Gardarein, Patrick. “EUROFAR Rotor Aerodynamic Tests.” Presented at the Eighteenth European Rotorcraft Forum, Avignon, France, September 15-18, 1992. Beziac, G. “Composite Blade for a 5-m Diameter Tilt Rotor.” Fourth European Rotorcraft and Powered Lift Aircraft Forum, Stresa, Italy, September 1978. Bilger, J.M.; Zahedi, A. “Results of Structural Dynamics Testing of the XV-15 Tilt Rotor Research Aircraft.” Journal of the American Helicopter Society, vol. 27, no. 2, April 1982. Bilger, J. M.; Marr, R. L.; Zahedi, Ahmed. “In-Flight Structural Dynamic Characteristics of the XV-15 Tilt Rotor Research Aircraft.” AIAA Paper 81-0612, 1981. Bilger, J. M.; Marr, R. L.; Zahedi, Ahmed. “Results of Structural Dynamic Testing of the XV-15 Tilt Rotor Research Aircraft.” Presented at the 37th Annual AHS Forum, New Orleans, Louisiana, May 1981. Bilger, J.; et al. “Interim Flight Test Data Report for XV-15 Tilt Rotor Research Aircraft (Flights 1–27, April–August 1979).” Bell Helicopter Textron Report No. 301-989-010, November 1979. Bondi, M. “Tilt Rotor—’Copter and Plane in One.” Mechanical Engineering, vol. 108, 1986.
Boorla, Raghupati. “Damage Tolerance Analysis of Dynamic Components of Rotary Wing Aircraft.” Journal of the American Helicopter Society, vol. 34, October 1989. Brandt, D. E. “Aeroelastic Problems of Flexible V/STOL Rotors.” AGARD CP No. 46, April 1969. Brieger, John T.; Maisel, Martin D.; Gerdes, Ronald. “External Noise Evaluation of the XV-15 Tilt Rotor Aircraft.” AHS National Specialists’ Meeting on Aerodynamics and Aeroacoustics, Arlington, Texas, February 25–27, 1987. Brigadier, William L. “Analysis of Control Actuator Authority Requirements for Attitude and Translational Rate Command Augmentation Systems for the XV-15 Tilt Rotor Research Aircraft.” NASA TM-81,243 (AVRADCOM Technical Report TR-80-A-13), 1980. Brown, J. H.; Edenborough, H. K.; “XV-15 Tilt Rotor Test Status.” Presented at the 33rd Annual National Forum of the AHS, Washington, DC, AHS Paper No. 77.33-64, May 1977. Brown, J. H.; Edenborough, H. K.; Few, D. D. “XV-15 Tilt Rotor Progress Report.” Presented at the Aerospace Meeting of the SAE, Los Angeles, California, SAE Paper No. 770953, November 14-17, 1977. Brown, J. H.; Edenborough, H. K.; Wernicke, K. G. “Evaluation of the Tilt Rotor Concept—The XV-15’s Role.” Presented at the Flight Mechanics Panel Symposium on Rotorcraft Design of the AGARD, Moffett Field, California, AGARD Paper No. 16, May 1977. Calise, A. J.; Rysdyk, R. “Research in Nonlinear Flight Control for Tilt Rotor Aircraft Operating in the Terminal Area.” NASA CR-203112, 1996. Carpenter, R. B.; Ball, J. C.; Becker, C. “XV-15 Experience—Joint Service Operational Testing of an Experimental Aircraft.” SETP, Report to the Aerospace Profession; Proceedings of the 27th Symposium, Beverly Hills, California, September 28–October 1, 1983. Carpenter, Ronald B.; Churchill, Gary B. “The XV-15 Experience from Wind Tunnel and Simulations to Joint Services V/STOL Aircraft.” Presented at the Army Operations Research Symposium, Ft. Eustis, Virginia, October 4–5, 1983. Cerbe, T. M.; Reichert, G.; Schrage, D. P. “Short Takeoff Optimization for the XV-15 Tilt Rotor Aircraft.” European Rotorcraft Forum, Berlin, Germany, September 24–26, 1991. 167
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
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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
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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 190 and 191: 164 Appendix F—Bibliography Tilt
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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