Wings

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Anderson Jr, John D., Corda Stephen and Van Wie, David M., Numerical Lifting Line Theory Applied to Drooped Leading-Edge Wings Below and Above Stall, J. Aircraft, Vol. 17, No. 12, Dec. 1980, pp. 898-904.

Ando, Shigenori, and Ichikawa, Akio, The Use of an Error Index to Improve Numerical Solutions for Unsteady Lifting Airfoils, AIAA J., Vol. 21, No. 1, Jan. 1983, pp. 47-54.

Ardonceau, P.L., Aerodynamic Properties of Crescent Wing Planforms, J. Aircraft, Vol.31, No. 2, 1993, pp. 462-465.

Arieli, R., Tauber, M., Saunders, D., Caughey, D., Computation of Transonic Flow About Helicopter Rotor Blades, AIAA Journal, May 1986.

Asai, Keisuke, Theoretical Considerations in the Aerodynamic Effectiveness of Winglets, J. Aircraft, Vol. 22 no. 7, July 1985, pp. 635-637.

Ashenberg, J. and Weihs, D., Minimum Induced Drag of Wings with Curved Planform, J. Aircraft, Vol. 21, No. 2, 1984, pp. 89-91.

Ashley, Holt and Rodden, William P., Wing-Body Aerodynamic Interaction, 1972.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Barber, T.J., An Investigation of Strut-Wall Intersection Losses, J. Aircraft, Vol. 15 no. 10, Oct. 1978, pp. 676-681.

Bauer, F., Garabedian, P., Korn, D., Jameson, A., Supercritical Wing Sections II, Sringer-Verlag, Berlin, 1975.

Boersma, J., Note on the lifting-surface problem for a circular wing in incompressible flow, Quarterly Journal of Mechanics and Applied Mathematics, 42, 1989, pp. 55-64.

Burkett, C.W., Reductions in induced drag by the use of aft swept wing tips, Aeronautical Journal, Dec. 1989, pp 400-405.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Carmichael, R., A Computer Program for the Estimation of the Aerodynamics of Wing Body Combinations, NASA Ames Research Center, 1969.

Cary, M.D., A Parametric Analysis of Winglet Effects, M.S. Thesis, Air Force Institute of Technology, Wright-Patterson AFB, OH, Dec. 1976.

Cheng, H.K. and Murillo, Luis E., Lunate-tail Swimming Propulsion as a Problem of Curved Lifting Line in Unsteady Flow. Part 1. Asymptotic Theory, J. Fluid Mechanics, Vol. 143., pp. 327-350.

Chopra, M.G., Hydrodynamics of lunate-tail swimming propulsion, J. Fluid Mech., Vol. 64, part 2, pp. 375-391.

Chopra, M.G., Large Amplitude Lunate-Tail Theory of Fish Locomotion, J. Fluid Mech., Vol. 74, part 1, pp. 161-182.

Clements, H.R., Canted Adjustable End Plates for the Control of Drag, Aeronautical Eng. Review, Vol. 14, No. 7, July 1955.

Cone, Clarence D., The Theory of Induced Lift and Minimum Induced Drag of Nonplanar Lifting Systems, NASA TR R-139, 1962. 31 pp.

Collins, L., Saunders, D., PROFILE User's Guide, Informatics General Corp. Technical Note No. 11, Nov. 1984.

Crittenden, J., et al., Aeroelastic Stability Characteristics of an Oblique-Wing Aircraft, J. Aircraft, July 1978.

Curry, R., Sims, A., Unique Flight Characteristics of the AD-1 Oblique-Wing Research Airplane, J. Aircraft, June 1983.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Dahlin, J.A., Aerodynamic Evaluation of Winglets for Transport Aircraft, AIAA Paper 81-1215, June 1981.

De Jarnette, Fred R., Arrangement of Vortex Lattices on Subsonic Wings in, Vortex-Lattice Utilization, NASA SP-405, 1976, pp. 301-323.

Devenport, William J and Simpson, Roger L., Flow Past a Wing- Body Junction - Experimental Evaluation of Turbulence Models, AIAA J., Vol. 30, no. 4, April 1992.

Devenport, William J., Agarwal, N.K., Dewitz, M.B., Simpson, Roger L. and Poddar, K., Flow Past a Wing-Body Junction - Experimental Evaluation of Turbulence Models, AIAA J., Vol. 30, no. 4, April 1992.

De Young, John, Induced Drag Ideal-Efficiency Factor of Arbitrary Lateral-Vertical Wing Forms, NASA Contractors Report, No. 3357, Dec. 1980, 47pp..

Dulikravitch, George S., Aerodynamic Shape Design and Optimization: Status and Trends, J. Aircraft, Vol. 29, No. 6, Nov.-Dec. 1992.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Eliraz, Y. and Ilan, D., Performance of the ARAVA Aircraft with Wing-Tip Winglets, Israeli J. Technology, Vol. 15, no. 1 and 2, 1977, Proc. of the 19th Israeli Annual Conf. on Aviation and Astronautics, Tel Aviv and Haifa, Israel, May 2-3, 1977, pp. 35-43.

Epton, Michael A., Integration by Parts Formula for Boundary- Element Methods, AIAA J., VOl. 30, No. 2, Feb. 1992, pp. 496-504.

Ermolenko, S.D., Rogozin, Yu.A. and Rogachev, G.V., Calculation of Aerodynamic Characteristics of a Rectangular Wing with Endplates near a Screen, Soviet Aeronautics, Vol. 18, no. 2, 1975.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Flechner, S.G., et al A High Subsonic Speed Wind-Tunnel Investigation of Winglets on a Representative Second- Generation Jet Transport Wing, NASA TN D-8264, 1976.

Flechner, S.G., Part VI - Stability Characteristics of a Full- Span Model at Subsonic Speeds, NASA TP-1330, 1979.

Fornasier, L., A Source-Equality Kutta Condition for Panel Methods, Vol. 22, No. 8, Aug. 1984, pp. 1167-1168.

Frink, Neal T., Lifting-Surface Theory for Skewed and Swept Wings, J. Aircraft, Vol. 19, No. 7, July 1982, pp. 519-524.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Gall, Peter D. and Smith, Hubert C., Aerodynamic Characteristics of Biplanes with Winglets, J. Aircraft, Vol. 24 no. 8, Aug. 1987, pp. 518-522.

Galloway, T., Gelhausen, P., Moore, M., Oblique Wing Supersonic Transport Concepts, AIAA 92-4230, August 1992.

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.

Graham, J.M.R., Effect of End-Plates on the Two-Dimensionality of a Vortex Wake, Aeronautical Quarterly, Vol. 20, part 3, Aug. 1969, pp. 237-247.

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.

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.

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.

Grasmeyer, Joel, A discrete vortex method for calculating the minimum induced drag and optimum load distribution for aircraft configurations with noncoplanar surfaces, VPI-AOE-242, Dept. Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University, Jan. 1997.

Guermond, J.-L., Collocation Methods and Lifting-Surfaces, European J. of Mechanics, B, Fluids, No. 4,1989, pp. 263-305.

Guermond, J.-L., A Generalized Lifting-line Theory for Curved and Swept Wings, J. Fluid Mech., Vol. 211, 1990, pp. 497-513.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Hancock, G.J., Comment on Spanwise Distribution of Induced Drag in Subsonic Flow by the Vortex Lattice Method, J. Aircraft, Vol. 8, No. 8, August 1971, pp. 681-682.

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.

Hauptman, A. and Miloh, T., On the exact solution of the linearized lifting-surface problem of an elliptic wing, Quarterly Journal of Mechanics and Applied Mathematics, 39, 1986, pp. 41-66.

Heltsley, Fred L., Report on the Status of a Slotted Wind-Tunnel Wall Representation Using the Vortex-Lattice Technique, in Vortex-Lattice Utilization, NASA SP-405,1976, pp. 145-162.

Heyson, H.H., Roebe, G.D. and Fulton, C.L., Theoretical Parametric Study of the Relative Advantages of Winglets and Wing-Tip Extensions, NASA TP 1020, 1977.

Hoerner, S.F., Fluid-dynamic Drag, published by the author, 1965.

Hough, Gary R., Remarks on Vortex-Lattice Methods, J. Aircraft, Vol. 10, No. 9, May 1973, pp. 314-316.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Ishimitsu, K.K., Aerodynamic design and analysis of winglets. AIAA Paper 76-940, Sept. 1976.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Jacobs, P.F., et al, Part I - Longitudinal Aerodynamic Characteristics of a Semi-Span Model at Subsonic Speeds, NASA TN D-8473, 1977.

Jacobs, P.F., Part V - Stability Characteristics of a Full- Span Wing with a Generalised Fuselage at High Subsonic Speeds, NASA TP-1163, 1978.

James, Richard M., On the Remarkable Accuracy of the Vortex Lattice Method, Computer Methods in Applied Mechanics and Engineering, Vol. 1, 1972, pp. 59-79.

Jameson, T., Transonic Flow Calculations for Airfoils and Bodies of Revolution, Aerodynamics Rpt. 390-71-1, Grumman Aerospace Corp.

Jones, R.T., Nisbet, J., Aeroelastic Stability and Control of an Oblique Wing, The Aeronautical Journal of the Royal Aeronautical Society, Aug. 1986.

Jones, R.T., The Minimum Drag of Thin Wings in Frictionless Flow, Journal of the Aeronautical Sciences, Feb. 1951.

Jones, R.T., Theoretical Determination of the Minimum Drag of Airfoils at Supersonic Speeds, Journal of the Aeronautical Sciences, Dec. 1952.

Jones, R.T., Aerodynamic Design for Supersonic Speed, Advances in Aeronautical Sciences, Vol.1, Pergammon Press, 1959.

Jones, R.T., New Design Goals and a New Shape for the SST, Astronautics and Aeronautics, Dec. 1972.

Jones, R.T., Nisbet, J., Transonic Transport Wings : Oblique or Swept?, Astronautics and Aeronautics, Jan. 1974.

Jones, R.T., The Oblique Wing : Aircraft Design for Transonic and Low Supersonic Speeds, Acta Astronautica, Vol. 4, Pergammon Press, 1977.

Jones, R.T., Cohen, D., High Speed Wing Theory, Princeton University Press, 1960.

Jones, R.T., The Flying Wing Supersonic Transport, Aeronautical Journal, March 1991.

Jordan, Peter F., Exact Solutions for Lifting Surfaces, AIAA Journal, Vol. 11, No. 8, Aug. 1973, pp. 1123-1129.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Karpouzian, G., Spedding, G. and Murillo, Luis E., Lunate-tail Swimming Propulsion. Part 2. Performance Analysis, J. Fluid Mechanics, Vol. 210, pp. 329-351.

Kroo, I., Tailless Aircraft Design: Recent Experiences, Ch. 7 of Aerodynamics and Aeroacoustics, K.Y. Fung, ed., March 1993.

Kroo, I., The Aerodynamic Design of Oblique Wing Aircraft, AIAA 86-2624, Sept. 1986.

Kucheman, D., The Aerodynamic Design of Aircraft, Pergammon Press, 1978.

Kuhlman, J.M., Cerney, M.J. and Liaw, P., Transonic Low Aspect Ratio Wing-Winglet Designs, AIAA Paper 88-0007, Jan. 1988.

Kuhlman, J.M., Liaw, P. and Cerney, M.J., Theoretical Numerical Study of Feasibility of Use of Winglets on Low Aspect Ratio Wings at Subsonic and Transonic Mach Numbers to Reduce Drag, NASA CR-4174, Aug. 1988.

Kuhlman, John M. and Liaw, Paul, Winglets on Low-Aspect Ratio Wings, J. Aircraft, Vol. 25 no. 10, Oct. 1988, pp. 932-941.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Laitone, E.V., Lift-curve slope for finite-aspect-ratio wings, J. Aircraft, Vol. 26, No. 8, Aug. 1989, pp. 789-790.

Lam, F. and Maull, D.J., Induced Drag of a Crescent Planform, J. Aircraft, Vol. 30, No. 5, Sept-Oct, 1993, pp. 594-602.

Lan, C.E., A Quasi-Vortex-Lattice Method in Thin Wing Theory, J. Aircraft, Vol. 11, No. 9, Sept. 1974, pp. 518-527.

Lan, C.E., Some Applications of the Quasi Vortex-Lattice Method in Steady and Unsteady Aerodynamics, Vortex-Lattice Utilization, NASA SP-405, 1976, pp. 385-405.

Lan, C.E., The Unsteady Quasi-vortex-lattice Method with Applications to Animal Propulsion, J. Fluid Mech., vol. 93, part 4, 1979,

pp. 747-765.

Lee, G.H., Slewed Wing Supersonics, The Aeroplane, March 1961.

Lombardi, G. and Vicini, A., Induced Drag Prediction for Wing-Tail and Canard Configurations through Numerical Optimisation, Aeronautical J., June/July 1994, pp. 199-206.

Lundry, J.L. and Lissaman, P.B.S., Minimum Induced Drag on Non-planar Wings, J. Aircraft, Vol. 5, No. 1, 1968, pp. 17-21.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Mangler, W., The Lift Distribution of Wings with End-Plates, NACA TM-856, 1938.

Mangler, K.W. and Smith, J.H.B., Bevaviour of the Vortex Sheet at the Trailing Edge of a Lifting Wing, Aeronautical Journal of the Royal Aeronautical Society, Nov. 1970, pp. 906-908.

Margason, R.J. and Lamar, J.E., Vortex-Lattice-Fortran Program for Estimating Subsonic Aerodynamic Characteristics of Complex Planforms, NASA TN D-6142, Feb. 1971.

Maskew, Brian, Prediction of Subsonic Aerodynamic Characteristics: A Case for Low-Order Panel Methods, J. Aircraft, Vol. 19, No. 2, Feb. 1982.

Meyer, R.R. Jnr et al, Part VII - Sideslip Effects on Winglet Loads and Selected Wing Loads at Subsonic Speeds for a Full-Span Model, NASA TP-2619, 1986.

Mineck, Robert E. and Vijgen, Paul M.H.W., Wind-tunnel investigation of aerodynamic efficiency of three planar elliptical wings with curvature of quarter-chord line, NASA TP-3359, 1993.

Montoya, L.C. et al, Part II - Pressure and Spanwise Load Distributions for a Semi-Span Model at High Subsonic Speeds, NASA TN D-8474, 1977.

Montoya, L.C. et al, Part III - Pressure and Spanwise Load Distributions for a Semi-Span Model at Mach 0.30, NASA TN D-8478, 1977.

Morris, S.J., Kroo, I., Aircraft Optimization with Dynamic Performance Constraints, J. Aircraft, Dec. 1990.

Munk, M.M., The Minimum Induced Drag of Aerofoils, NACA Report 121, 1921.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Naik, D.A. and Ostawari, C., Effects of Nonplanar Outboard Wing Forms on a Wing, J. Aircraft, Vol. 27, No. 2, Feb. 1990, pp. 117-122.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Pavelka, Jerry and Tatum, Kenneth, E., Validation of a Leading-Edge Stall Prediction Technique, J. Aircraft, Vol. 18, No. 10, Oct. 1981, pp. 849-854.

Potts, Jonathan R. and Crowther, William J., Flight control of a spin stabilised axi-symmetric disc-wing, AIAA 2001-0253.

Potts, J.R. and Crowther, W.J., Frisbee aerodynamics, AIAA 2002-3150, 20th AIAA Applied Aerodynamics Conference and Exhibit, 24-26 June 2002, St. Louis, Missouri.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Rech, J., Leyman, C.S., Concorde Aerodynamics and Associated Systems Development, in Case Studies in Aircraft Design, Published by AIAA, 1980.

Reynolds, Peter T., Winglets Introduced on Business Jets, Automotive Engineering, Vol. 87, no. 4, April 1979, pp. 44-47.

Rosen, Bruce S., Computational Transonic Analysis of Canted Winglets, J. Aircraft, Vol. 21, no. 11, Nov. 1984, pp. 873- 878.

Rossow, Vernon J., Lift Enhancement by an Externally Trapped Vortex, J. Aircraft, Vol. 15, No. 9, Sep. 1978, pp. 618-625.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Schlichting, Hermann and Truckenbrodt, Erich, Aerodynamics of the airplane, McGraw-Hill, 1979.

Shen, S.F. and Chan, Stevens T.K., Variational Approach to the Lifting Surface Equation, AIAA J., Vol. 11, No. 10, October 1973, pp. 1390-1395.

Shevell, R.S., Fundamentals of Flight, Prentice-Hall, 1983.

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.

Sim, A., Curry, R., Flight Characteristics of the AD-1 Oblique Wing Research Airplane, NASA TP 2223, March 1985.

Smith, J.H.B., Wing Tip Flows and Wing Devices (Symposium): Introductory Remarks, Aeronautical J., Dec. 1987, pp. 443-445.

Smith, J.S., Modelling Winglets Using the SPARV Computer Program, in Computational Methods in Aeronautical Fluid Dynamics, ed. P. Stow, Clarendon Press, Oxford, England, 1990.

Smith, Stephen C. and Kroo, Ilan, Computation of Induced Drag for Elliptical and Crescent-Shaped Wings, J. Aircraft, Vol. 30 no. 4, Jul-Aug. 1993, pp. 446-452.

Smith, J. H. B., Wing Tip Flows and Wing Devices (Symposium): Introductory Remarks, Aeronautical J., Dec. 1987, pp. 443-445.

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.

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.

Smith, J. H., Lift/Drag Ratios of Optimised Slewed Elliptic Wings at Supersonic Speeds, The Aeronautical Quarterly, August 1961.

Spillman, J. J., The Use of Wing Tip Sails to Reduce Vortex Drag, Aeronautical J., Sept. 1978, pp. 387-395.

Standingford, D.W.F. and Tuck, E.O., Lifting Surfaces in Ground Effect, Ekranoplans Workshop, 5-6 Dec., 1996, University of New South Wales, Australia.

Standingford, D.W.F., Optimal Lifting Surfaces (including Endplates, Ground Effect and Thickness), PhD Thesis, Dept. Applied Mathematics, The University of Adelaide, July 1997.

Stark, Valter J.E., A Generalised Quadrature Formula for Cauchy Integrals, AIAA J., Vol 9, No. 9, Sept. 1971, pp 1854-1855.

Stewartson, K., A Note on Lifting Line Theory, Quart. J. Mech. and Applied Math., Vol. 13, no. 1, 1960. pp. 49-56.

Stratford, B., The Prediction of Separation of the Turbulent Boundary Layer, J. Fluid Mech., Vol. 5, 1959.

Sugiyama, Y., A Theory for Rectangular Wings with Small Tip Clearance in a Channel, Aeronautical Quarterly, May 1973, pp. 103-119.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Takami, H., Kawakatsu, H. and Kubota, H., Optimization of the Spanwise Load Distribution of Wings with End-Plates for the Minimum Induced Drag, Proc. 14th JSASS Annual Conference, Tokyo, April 1983, pp. 12-13.

Tuck, E.O., A Nonlinear Unsteady One-Dimensional Theory for Wings in Extreme Ground Effect, J. Fluid Mech., Vol. 98, part 1, 1980, pp. 33-47.

Tuck, E.O., Lifting Surfaces with Endplates, 11th Australasian Fluid Mechanics Conf, Hobart, Australia, 14-18 Dec. 1992.

Tuck, E.O., Some Accurate Solutions of the Lifting Surface Integral Equation, J. Australian Math. Soc. Series B, No. 35, 1993, pp. 127-144.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Van der Velden, A., Kroo, I., A Numerical Method for Designing Wings Based on Two Dimensional Pressure Distributions, AIAA Aircraft Design Conference, Sept. 1990.

van Dam, Cornelis, P., Holmes, Bruce J. and Pitts, Calvin, Effect of Winglets on Performance and Handling Qualities of General Aviation Aircraft, J. Aircraft, Vol. 18, No. 7, Jul 1981., pp. 587-591.

van Dam, C.P., Analysis of Non-planar Wing-Tip-Mounted Lifting-Surfaces on Low-Speed Airplanes, NASA Contractors Report 3684, Jun. 1983, 174 pp.

van Dam, C.P., Natural Laminar Flow Airfoil Design Considerations for Winglets on Low-Speed Airplanes, NASA Contractors Report, 3853, Dec. 1984, 27 pp.

van Dam, C.P., Induced-Drag Characteristics of Crescent-Moon-Shaped Wings, J. Aircraft, Vol. 24, No. 2, Feb. 1987., pp. 115-119.

van Dam, C.P., Efficiency Characteristics of Crescent-shaped Wings and Caudal Fins, Nature, Vol. 325, 29 Jan. 1987, pp. 435-437. van Niekerk, Becker, Integration of Singular Functions Associated with Lifting Surface Theory, AIAA J., Vol. 24, No. 7, July 1986, pp. 1195-1196.

van Oossanen, P. and Joubert, P.N., The Development of the Winged Keel for Twelve-Metre Yachts, J. Fluid Mechanics, vol. 173, 1986, pp. 55-71.

Van der Velden, A., Kroo, I., The Sonic Boom of an Oblique Flying Wing, Journal of Aircraft, Jan. 1994.

Vijgen, P.M.H.W., van Dam, C.P. and Holmes, B.J., Sheared Wing-Tip Aerodynamics: Wind Tunnel and Computational Investigation, J. Aircraft, Vol. 26, No. 3, March 1989, pp. 207-213.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Wakayama, Sean, and Kroo, Ilan, Subsonic Wing Planform Design Using Multidisciplinary Optimization, J. Aircraft, Vol. 12, No. 4, Jul.-Aug. 1995, pp. 746-753.

Weisshaar, T., Crittenden, J., Flutter of Asymmetrically Swept Wings, AIAA Journal, Aug. 1976.

Weisshaar, T., Zeiler, T., Dynamic Stability of Flexible Forward Swept Wing Aircraft, J. Aircraft, Dec. 1983.

Whitcomb, R. T., A Design Approach and Selected Wind-Tunnel Results at High Subsonic Speeds for Wing-tip Mounted Winglets, NASA TN D-8260, 1976.

Whitcomb, R.T., Methods for Reducing Subsonic Drag Due to Lift, AGARD Report no. 654, Special Course on Concepts for Drag Reduction, Von Karman Institute, Rhode-St-Genese, Belgium, Mar 28-April 1, 1977, Published by AGARD, Neuilly sur Seine, France, Jun 1977, pp. 2.1-2.17.

Woodward, F., Analysis and Design of Wing-Body Combinations at Subsonic and Supersonic Speeds, J. Aircraft, Dec. 1968.

A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

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