Oblique Wing Bibliography


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 Experimantal
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 Compute
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. Morris, S., Tigner, B.,  "Flight Tests of an Oblique Flying Wing Small 
Scale Demonstrator", AIAA paper No. 95-3327-CP,  Guidance, Navigation and 
Control Conference, August, 1995, Baltimore, MD.