References for the Vortex Lattice Minimum Drag Program
The first item is the primary reference for this program.
Lamar, John E.:
A Vortex-Lattice Method for the Mean Camber Shapes
of Trimmed Noncoplanar Planforms with Minimum Vortex Drag.
,
NASA Technical Note D-8090, June 1976.
Lamar, John E.:
A Modified Multhopp Approach for Predicting Lifting Pressures and
Camber Shape for Composite Planforms in Subsonic Flow.
NASA Technical Note D-4427, July 1968, and
Supplement to D-4427.
Carlson, Harry W.; and Middleton, Wilbur D.:
A Numerical Method for the Design of Camber Surfaces of
Supersonic Wings With Arbitrary Planforms.
NASA Technical Note D-2341, June 1964.
Sorrells, Russell B.; and Miller, David S.:
Numerical Method for Design of Minimum-Drag Supersonic Wing Camber
With Constraints on Pitching Moment and Surface Deformation.
NASA Technical Note D-7097, December 1972.
Margason, Richard J.; and Lamar, John E.:
Vortex-Lattice FORTRAN Program for Estimating Subsonic Aerodynamic
Characteristics of Complex Planforms.
NASA Technical Note D-6142, February 1971.
Lundry, J. L.:
A Numerical Solution for the Minimum Induced Drag, and the
Corresponding Loading, of Nonplanar Wings.
NASA Contractor Report 1218, November 1968.
Loth, John L.; and Boyle, Robert E.:
Optimum Loading on Nonplanar Wings at Minimum Induced Drag.
Aerosp. Eng. TR-19 (Contract N00014-68-A-1512), West
Virginia Univ., Aug. 1969. (Available from DDC as AD 704 502.)
Munk, Max M.:
The Minimum Induced Drag of Aerofoils.
NACA Report 121, 1921.
Milne-Thomson, L. M.: Theoretical Aerodynamics.
Second ed. D. Van Nostrand Co., Inc., 1952.
Abbott, Ira H.; Von Doenhoff, Albert E.; and Stivers, Louis S., Jr.:
Summary of Airfoil Data.
NACA Report 824, 1945. (Supersedes NACA WR L-560.)
Katzoff, S.; Faison, M. Frances; and DuBose, Hugh C.:
Determination of Mean Camber Surfaces for Wings Having Uniform Chordwise
Loading and Arbitrary Spanwise Loading in Subsonic Flow.
NACA Report 1176, 1954. (Supersedes NACA TN 2908.)
Henderson, William P.:
Pressure Distributions on a Cambered Wing-Body Configuration
at Subsonic Mach Numbers.
NASA Technical Note D-7946, July 1975.
Henderson, William P.; and Huffman, Jarrett K.:
Effect of Wing Design on the Longitudinal Aerodynamic Characteristics
of a Wing-Body Model at Subsonic Speeds.
NASA Technical Note D-7099, 1972.
Henderson, William P.; and Huffman, Jarrett K.:
Aerodynamic Characteristics of a Tandem Wing Configuration
at a Mach Number of 0.30.
NASA Technical Memorandum X-72779, October 1975.
Carmichael, Ralph L.; Castellano, Charles R.; and Chen, Chuan F.:
The Use of Finite Element Methods for Predicting the Aerodynamics of
Wing-Body Combinations.
Analytic Methods in Aircraft Aerodynamics, NASA Special Publication 228, 1969, pp. 37-51.
Rubbert, P. E.; Saaris, G. R.; Scholey, M. B.; Standen, N. M.; and Wallace, R. E.:
A General Method for Determining the Aerodynamic Characteristics of
Fan-in-Wing Configurations. Vol. I - Theory and Application.
USAAVLABS Tech. Rep. 67-61A, U.S. Army, Dec. 1967.
Rubbert, Paul E.:
Theoretical Characteristics of Arbitrary Wings by a Non-Planar
Vortex Lattice Method.
Doc. No. D6-9244, Boeing Co., Feb. 1964.
Hedman, Sven G.:
Vortex Lattice Method for Calculation of Quasi Steady State
Loadings on Thin Elastic Wings in Subsonic Flow.
FFA Rep. 105, Aeronaut. Res. Inst. Swed., 1966.
James, R. M.:
On the Remarkable Accuracy of the Vortex Lattice Discretization in
Thin Wing Theory.
Rep. No. DAC 67211, McDonnell Douglas, Feb. 1969.
Giesing, Joseph P.:
Lifting Surface Theory for Wing-Fuselage Combinations.
Rep. DAC-67212, Vol. I, McDonnell Douglas, Aug. 1, 1968.
Belotserkovskii, S. M.:
Special Features of Subsonic Flow Past Wings of Complex Plan-Form.
Libr. Transl. 1297, Brit. R.A.E., Apr. 1968.
Dulmovits, John:
A Lifting Surface Method for Calculating Load Distributors and the
Aerodynamic Influence Coefficient Matrix for Wings in Subsonic Flow.
Rep. No. ADR 01-02-64.1, Grumman Aircraft Eng. Corp., Aug. 1964.
Albano, Edward; and Rodden, William P.:
A Doublet-Lattice Method for Calculating Lift Distributions on Oscillating
Surfaces in Subsonic Flows.
AIAA Journal, vol. 7, no. 2, Feb. 1969, pp. 279-285.
Woodward, Frank A.:
Analysis and Design of Wing-Body Combinations at Subsonic and Supersonic Speeds.
Journal of Aircraft, vol. 5, no. 6, Nov.-Dec. 1968, pp. 528-534.
Campbell, George S.:
A Finite-Step Method for the Calculation of Span Loadings of Unusual Plan Forms.
NACA Research Memorandum L50L13, 1951.
Blackwell, James A., Jr.:
A Finite-Step Method for Calculation of Theoretical Load Distributions
for Arbitrary Lifting-Surface Arrangements at Subsonic Speeds.
NASA Technical Note D-5335, 1969.