Advanced Design Studies and Unusual Concepts

Oblique Wing Concepts

from the Virginia Tech Aircraft Design Information Sources pages

Robert T. Jones and James W. Nisbet, “Transonic Transport Wings-Oblique or Swept?” Astronautics and Aeronautics, Jan. 1974, pp. 40-47. They really mean supersonic transports, but couldn't say so.

Terrance A weisshaar and J. B. Crittenden, “Flutter of Asymetrically Swept Wings” AIAA Journal, Vol. 14, No. 8, August 1976, pp, 993-994.

Walter P. Nelms, Jr., “Applications of Oblique-Wing Technology-An Overview,” AIAA Paper 76-943, Sept. 1976.

J. B. Crittenden, T.A. Weisshaar, E.H. Johnson and M.J. Rutkowski, “Aeroelastic Stability Characteristics of an Oblique-Wing Aircraft,” Journal of Aircraft, Vol. 15, No. 7, July 1978, pp. 429-434.

Georgr H. Kidwell, Jr., “Conceptual Design Study of Subsonic V/STOL and STOVL Aircraft Derivatives of the S-3A,” NASA TM 81310, July, 1981. This includes a study of an oblique wing version.

C.D. Wiler and S.N. White, “Projected Advantage of an Oblique Wing Design on a Fighter Mission,” AIAA Paper 84-2474, Oct.-Nov. 1984.

Ilan Kroo, “The Aerodynamic Design of Oblique Wing Aircraft,” AIAA 86-2624, Oct. 1986. This paper also has an extensive list of references.

Terrence A. weisshaar and Jonathan M. Bohlmann, “Supersonic Flutter of Aeroelastically Tailored Oblique WIngs,” AIAA Paper 87-0734.

Alex J. M. Van der Velden and E. Torebeek, “Design of a Small Supersonic Oblique- Wing Transport Aircraft,” Journal of Aircraft, Vol. 26, No. 3, Mar. 1989, pp.193-197.

Jonathan G. Bohlmann, Clinton V. Eckstrom and Terrence A. Weisshaar, “Static Aeroelastic Tailoring for Oblique Wing Lateral Trim,” Journal of Aircraft, Vol. 27, No. 6, June 1990, pp. 558-563.

Van der Velden, A., “Aerodynamic Design and Synthesis of the Oblique Flying Wing Supersonic Transport,” PH.D. Dissertation, SUDDAR 621, Stanford Univ., Stanford, CA, May 1992.

Tom Galloway, Paul Gelhausen, and Mark Moore, “Oblique Wing Supersonic Transport Concepts,” AIAA Paper 92-4230, Aug. 1992.

A. Van der Velden, “Multi-Disciplinary SCT Design Optimization,” AIAA Paper 92-3931, Aug. 1993.

A. Van der velden and I. Kroo, “Sonic Boom of the Oblique Flying Wing,” Journal of Aircraft, Vol. 31, No. 1, Jan.-Feb. 1994, pp. 19-25.

Terrence A. Weisshaar, “Integrated Structure/Control Concepts for Oblique Wing Roll Control and Trim,” Journal of Aircraft, Vol. 31, No. 1, Jan.-Feb. 1994, pp. 117- 124.

Stephen J. Morris and Benjamin Tigner, “Flight Tests of an Oblique Flying Wing Small Scale Demonstrator,” AIAA Paper 95-3327. Sept. 1994?

Pei Li, Richard Seebass and Helmut Sobieczky, “Oblique flying wing aerodynamics,” AIAA Paper 96-2120. June 1996.

Blaine K. Rawdon, “Oblique All-Wing Airliner Sizing and Integration,” AIAA Paper 97-5568, 1997.

A.J.M. Van der Velden, “The Oblique Flying Wing Transport,” New Design Concepts for High Speed Transport, edited by H. Sobieczky, CISM Courses and Lectures, Vol. 366, Springer-Verlag, Vienna/New York, 1997, pp. 291-315.

Richard Seebass, “Oblique Flying Wing Studies,” New Design Concepts for High Speed Transport, edited by H. Sobieczky, CISM Courses and Lectures, Vol. 366, Springer-Verlag, Vienna/New York, 1997, pp. 317-336.

P. Li, Richard Seebass and H. Sobieczky, “Manual Aerodynamic Optimization of an Oblique Flying Wing,” AIAA Paper 98-0598.

Benjamin Tigner, Mark J. Meyer, Michael E. Holden, Blaine K. Rawdon, Mark A. Page, William Watson, and Ilan Kroo, “Test Techniques for Small-Scale Research Aircraft,” AIAA Paper 98-2726.

Pei Li, Helmut Sobieczky and Richard Seebass, “Manual Aerodynamic Optimization of an Oblique Wing Supersonic Transport,” Journal of Aircraft, Vol. 36, No. 6, Nov.-Dec. 1999, pp. 907- 913.

E. Livne and Rerrence A. Weisshaar, “Aeroe;asticity of Nonconventional Airplane Configurations - Past and Future,” ournal of Aircraft, Vol. 40, No. 6, Nov-Dec. 2003, pp. 1047-.

Melissa A. McDaniel and Brett L. Wilks, “Oblique Wing Aerodynamics,” AIAA Paper 2004-5194. Note: this is a cruise missile application.

Mathias Wintzer, Peter Sturdza and Ilan Kroo, “Conceptual Design of Conventional and Oblique Wing Configurations for Small Supersonic Aircraft, ” AIAA Paper 2006-930, Jan. 2006.

Michael J. Hirschberg, David M. Hart and Thomas J. Beutner, “A Summary of a Half-Century of Oblique Wing Research,” AIAA Paper 2007-150, 2007.

Lei Tang, Danny D. Liu and P.C. Chen, “Extension of Projectile Range Using Oblique-Wing Concept,” Journal of Aircraft, Vol. 44, No. 3, May-June 2007. pp. 774- .

R. K. Nangia and M. E. Palmer, “Formation Flying of Oblique Wing Aircraft, Assessment of Variations in Formation Configuration - Induced Effects and Control” AIAA Paper 2007-4569. June 2007.

R.K. Nangia, M.E. Palmer, William Blake and C. P. Tilmann, “Exploiting Formation Flying for Fuel Savings - Supersonic Oblique Wings,” AIAA Paper 2008-0202. Jan. 2008.

Ryan Plumley, “Conceptual Assessment of an Oblique Flying Wing Aircraft Including Control and Trim Charateristics,” MS Thesis, Virginia Tech, February, 2008. See his thesis for a comprehensive bibliography.

Susan E. Cliff, Scott D. Thomas and Veronica M. Hawke, “Swing-WIng Inline-Fuselage Transport Design Studies at Supersonic Flight Conditions,“ AIAA Paper 2009-7073, Sept. 2009.

for a complete bibliography through 1995, see the oblique wing bibliography on the world wide web at Ilan Kroo's group's page under Reports: http://aero.stanford.edu/ADG.html

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direct comments and suggestions to W.H. Mason, whmason@vt.edu