1. Taylor, J., Munson, K., ed. History of Aviation, Crown Publishers, Inc., 1978 (Picture of Blohm and Voss Oblique Wing)
2. Kucheman, D., The Aerodynamic Design of Aircraft, Pergammon Press, 1978
3. Tennant, R., "Super-Sonic Developments", The Aeroplane, Feb.7, 1947
4. Campbell, J., Drake, H., "Investigation of Stability and Control Characteristics of an Airplane Model with a Skewed Wing in the Langley Free Flight Tunnel", NACA Technical Note 1208, May 1947
5. Jones, R.T., "The Minimum Drag of Thin Wings in Frictionless Flow," Journal of the Aeronautical Sciences, Feb. 1951
6. Jones, R.T., "Theoretical Determination of the Minimum Drag of Airfoils at Supersonic Speeds," Journal of the Aeronautical Sciences, Dec. 1952
7. Jones, R.T., "Possibilities of Efficient High Speed Transport Airplanes," Proceedings of the Conference on High-Speed Aeronautics, Polytechnic Institute of Brooklyn, Jan. 1955
8. Jones, R.T., "Aerodynamic Design for Supersonic Speed," Advances in Aeronautical Sciences, Vol.1, Pergammon Press, 1959
9. Lee, G.H., "Slewed Wing Supersonics," The Aeroplane, March 1961
10. Jones, R.T., "New Design Goals and a New Shape for the SST," Astronautics and Aeronautics, Dec. 1972
11. Jones, R.T., Nisbet, J., "Transonic Transport Wings -- Oblique or Swept?" Astronautics and Aeronautics, Jan. 1974
12. Jones, R.T., "The Oblique Wing -- Aircraft Design for Transonic and Low Supersonic Speeds," Acta Astronautica, Vol. 4, Pergammon Press, 1977
13. Jones, R.T., Cohen, D., High Speed Wing Theory, Princeton University Press, 1960
14. Rech, J., Leyman, C.S., "Concorde Aerodynamics and Associated Systems Development," in Case Studies in Aircraft Design, Published by AIAA, 1980
15. Taylor, J., ed., Jane's All the World's Aircraft 1984-85, Jane's Publishing Co. Ltd., 1985
16. Wiler, C., White, S., "Projected Advantage of an Oblique Wing Design on a Fighter Mission," AIAA-84-2474, Nov. 1984
17. Curry, R., Sims, A., "Unique Flight Characteristics of the AD-1 Oblique-Wing Research Airplane," J. Aircraft, June 1983
18. Kulfan, R.M., et al., "High Transonic Speed Transport Aircraft Study," Fional Report, NASA CR-114658, 1973
19. Jones, R.T., Nisbet, J., "Aeroelastic Stability and Control of an Oblique Wing," The Aeronautical Journal of the Royal Aeronautical Society, Aug. 1986
20. Weisshaar, T., Crittenden, J., "Flutter of Asymmetrically Swept Wings," AIAA Journal, Aug. 1976
21. Crittenden, J., et al., "Aeroelastic Stability Characteristics of an Oblique-Wing Aircraft," J. Aircraft, July 1978
22. Weisshaar, T., Zeiler, T., "Dynamic Stability of Flexible Forward Swept Wing Aircraft," J. Aircraft, Dec. 1983
23. Nelms, W., "Applications of Oblique Wing Technology -- An Overview," AIAA 76-943, Sept. 1976
24. Bradley, E., et al., "An Analytical Study for Subsonic Oblique Wing Transport Concept," Fianl Report, NASA CR 137896, 1976
25. BCAC Preliminary Design Dept., "Oblique Wing Transonic Transport Configuration Development," Final Report, NASA CR 151928, 1977
26. Kulfan, J., "Study of the Single-Body Yawed Wing Aircraft Concept," NASA CR 137483, 1974
27. Graham, A., Jones, R.T., Boltz, F., "An Experimental Investigation of an Oblique Wing and Body Combination at Mach Numbers Between .6 and 1.4," NASA TM X-62207, Dec. 1972
28. Graham, A., Jones, R.T., Boltz, F., "An Experimental Investigation of Three Oblique Wing and Body Combinations at Mach Numbers Between .6 and 1.4," NASA TM X-62256, April 1973
29. Hopkins, E., Nelson, E., "Effect of Wing Bend on the Experimental Force and Moment Characteristics of an Oblique Wing," NASA TM X-3343, March 1976
30. Black, R., Beamish, J., Alexander,W., "Wind Tunnel Investigation of an Oblique Wing Transport Model at Mach Numbers Between .6 and 1.4," NASA CR-137697, July 1975
31. Bailey, R., Putnam, P., "Oblique Wing Remotely Piloted Research Aircraft," Presented at 1975 Meeting of the National Assoc. for Remotely Piloted Vehicles, June 1975
32. Andrews, W., et al., "AD-1 Oblique Wing Aircraft Program," SAE Paper No. 801180, Oct. 1980
33. White, S., Beeman, E., "Future Oblique Wing Designs," SAE Paper No. 861643, Oct. 1986
34. White, S., et al., "A Feasibility Design Study for an F-8 Oblique Wing Research Demonstrator," Final Report, NASA Contract No. NAS-11409, July 1984
35. Graham, A., Jones, R.T., Summers, J., "Wind Tunnel Test of an F-8 Airplane Model Equipped with an Oblique Wing," NASA TM X-62273, June 1973
36. Smith, R., Jones, R.T., Summers, J., "Transonic Wind Tunnel Tests of an F-8 Airplane Model Equipped with 12 and 14-percent Thick Oblique Wings," NASA TM X-62478, Oct. 1975
37. Smith, R., Jones, R.T., Summers, J., "Transonic Longitudinal and Lateral Control Characteristics of an F-8 Airplane Model Equipped with an Oblique Wing," NASA TM X-73103, March 1976
38. NASA Ames Research Center, "Oblique Wing Research Aircraft Preliminary Design (RFP)," RFP2-31666, Nov. 1984
39. Smith, J. H., "Lift/Drag Ratios of Optimised Slewed Elliptic Wings at Supersonic Speeds," The Aeronautical Quarterly, August 1961
40. Bauer, F., Garabedian, P., Korn, D., Jameson, A., Supercritical Wing Sections II, Sringer-Verlag, Berlin, 1975
41. Kennelly, R., "Wind Tunnel Test of a 12% Thick High Lift Transonic Airfoil," NASA CR in press, 1986
42. Kennelly, R., "Improved Method for Transonic Design-By-Optimization," AIAA Paper No. 83-1864, July 1983
43. Jameson, T., "Transonic Flow Calculations for Airfoils and Bodies of Revolution," Aerodynamics Rpt. 390-71-1, Grumman Aerospace Corp
44. Gill, P., Murray, W., Pitfield, R., "The Implementation of Two Revised Quasi-Newton Algorithms for Unconstrained Optimization," National Physical Laboratory Rpt. NAC 11, April 1972
45. Stratford, B., "The Prediction of Separation of the Turbulent Boundary LAyer," J. Fluid Mech., Vol. 5, 1959
46. Collins, L., Saunders, D., PROFILE User's Guide, Informatics General Corp. Technical Note No. 11, Nov. 1984
47. Harris, C., "Aerodynamic Characteristics of a 14-Percent-Thick Airfoil Designed for a Normal Force Coefficient of 0.7," NASA TM X-72712, July 1975
48. Sidewell, K., Baruah, P., Bussoletti, J., "PAN AIR -- A Computer Program for Predicting Subsonic or Supersonic Linear Potential Flows About Arbitrary Configurations Using a Higher Order Panel Method. Vol II, User's Manual," NASA CR-3252, 1980
49. Carmichael, R., "A Computer Program for the Estimation of the Aerodynamics of Wing Body Combinations," NASA Ames Research Center, 1969
50. Woodward, F., "Analysis and Design of Wing-Body Combinations at Subsonic and Supersonic Speeds", J. Aircraft, Dec. 1968
51. Arieli, R., Tauber, M., Saunders, D., Caughey, D., "Computation of Transonic Flow About Helicopter Rotor Blades," AIAA Journal, May 1986
52. Mehta, U., "The Computation of Flow Past an Oblique Wing Using the Thin-Layer Navier-Stokes Equations," NASA TM 88317, June 1986
53. Alag, G., Kempel, R., Pahle, J., "Decoupling Control Synthesis for an Oblique-Wing Aircraft," NASA TM 86801, June 1986
54. Burken, J., Alag, G., Gilyard, G., "Aeroelastic Control of Oblique-Wing Aircraft," NASA TM 86808, June 1986
55. Barber, M., DeAngelis, M., Traskos, R., "F-8 Oblique Wing Research Aircraft - A Progress Report," Society of Flight Test Engineers 17th Annual Symposium, August 1986
56. Kroo, I., "The Aerodynamic Design of Oblique Wing Aircraft," AIAA 86-2624, Sept. 1986
57. Morris, S.J., Kroo, I., "Aircraft Optimization with Dynamic Performance Constraints," J. Aircraft, Dec. 1990
58. Phillips, J., "Modal Control of an Oblique Wing Aircraft," NASA TP 2898, Jan. 1989
59. Morris, S.J., "Integrated Aerodynamics and Control System Design for Oblique Wing Aircraft," Ph.D. Thesis, Stanford University, June 1990.
60. Kempel,R., McNeill, W., Gilyard, G., Maine, T., "A Piloted Evaluation of an Oblique Wing Research Aircraft Motion Simulation with Decoupling Control Laws," NASA TP 2874, Nov. 1988.
61. Curry, R., Sim, A., "In-Flight Total Forces, Moments, and Static Aeroelastic Characteristics of an Oblique Wing Research Airplane," NASA TP 2224, Oct. 1984.
62. Curry, R., Sim, A., "Flight-Determined Aerodynamic Derivatives of the AD-1 Oblique Wing Research Airplane," NASA TP 2222, Oct. 1984.
63. Sim, A., Curry, R., "Flight Characteristics of the AD-1 Oblique Wing Research Airplane," NASA TP 2223, March 1985.
64. Van der Velden, A., Kroo, I., "The Sonic Boom of an Oblique Flying Wing," Journal of Aircraft, Jan. 1994.
65. van der Velden, A., Kroo, I., "Aerodynamic Design of the Oblique Flying Wing Supersonic Transport," NASA CR 177552, June 1990.
66. Kennelly, R., Kroo, I., Strong, J., Carmichael, R., "Transonic Wind Tunnel Test of a 14% Thick Oblique Wing," NASA TM 102230, August 1990.
67. Van der Velden, A., Kroo, I., "A Numerical Method for Designing Wings Based on Two Dimensional Pressure Distributions," AIAA Aircraft Design Conference, Sept. 1990.
68. Jones, R.T., "The Flying Wing Supersonic Transport," Aeronautical Journal, March 1991.
69. Tauber, M., Langhi, R., Transonic Rotor Tip Design Using Numerical Optimization, NASA TM-86771, October 1985.
70. Waters, Ardema, Roberts, Kroo,"Structural and Aerodynamic Considerations for an Oblique All-Wing Aircraft," AIAA 92-4220, AIAA Aircraft Design Meeting, August 1992.
71. Seebass, A. R., "The Prospects for Commercial Transprot at Supersonic Speeds," AIAA 94-0017, Sixth Biannual W.F. Durand Lecture, Arlington, VA, May 1994.
72. Galloway, T., Gelhausen, P., Moore, M., "Oblique Wing Supersonic Transport Concepts," AIAA 92-4230, August 1992.
73. Kroo, I., "Tailless Aircraft Design -- Recent Experiences," Ch. 7 of Aerodynamics and Aeroacoustics, K.Y. Fung, ed., March 1993.
74. Sobieczky, H., ed., New Design Concepts for High Speed Air Transport, Springer, 1997.