Agnone, Anthony M., "Using MathCAD in Aircraft Design Instruction", Session 0011, 100th Annual ASEE Conf. & Centennial Celebration, June 1993.
Axelson, J.A., "AEROX - Computer Program for Transonic Aircraft Aerodynamics to High Angles of Attack," Vol. I - Aerodynamics Methods & Program User's Guide, Vol. II - Comparisons of Test Cases with Experiment, Vol. III - AEROX Computer Program Listing, NASA TM X-73,208, Feb. 1977.
Axelson, John A., "Estimation of Transonic Aircraft Aerodynamics to High Angles of Attack," Journal of Aircraft, Vol. 14, No. 6, June 1977, pp.553-559.
Axelson, J.A., and Hill, G.C., "Comparisons of AEROX Computer Program Predictions of Lift and Induced Drag with Flight-Test Data," NASA TM 81237, Aug. 1981.
Blake, W.B., "Prediction of Fighter Aircraft Dynamic Derivatives Using Digital DATCOM," AIAA Paper No. 85-4070, October, 1985.
Crawford, Donald R., A Practical Guide to Airplane Performance and Design, Crawford Aviation, 1984.
Crawford, Donald R., Airplane Design, Crawford Aviation, Torrance, CA, 1986
Drela, Mark, "XFOIL: An Analysis and Design System for Low Reynolds Number Airfoils," in Low Reynolds Number Aerodynamics, T.J. Mueller, editor. Lecture Notes in Engineering #54, Springer-Verlag, 1989
Einthoven, Pieter, "Aircraft Handling Qualities Evaluation Software, for use with MATLAB: Background and User's Manual," Virginia Tech Aerospace and Ocean Engineering Report, Dec. 12, 1994.
Goodrich, K. H., Sliwa, S. M., and Lallman, F. J., "A Closed-form Trim Solution Yielding Minimum Drag for Airplanes with Multiple Longitudinal Control Effectors," NASA TP-2907, May 1989.
Gregory, T.J., "Computerized Preliminary Design at the Early Stages of Vehicle Definition," in Aircraft Design Integration and Optimization, AGARD CP-147, 1974.
Jayaram, S., Myklebust, A., and Gelhausen, P., "ACSYNT - A Standards-Based System for Parametric Computer Aided Conceptual Design of Aircraft," AIAA Paper 92-1268, Feb. 1992.
Kay, J., Mason, W.H. , Lutze, F., and Durham, W., "Control Authority Issues in Aircraft Conceptual Design," AIAA Paper 93-3968, August 1993.
Kay, Jacob , Mason, W.H. , Durham, W. , Lutze, F. and Benoliel, A. , "Control Power Issues in Conceptual Design: Critical Conditions, Estimation Methodology, Spreadsheet Assessment, Trim and Bibliography," VPI-Aero-200, November 1993.
Krenkel, A.R., and Salzman, A., "Takeoff Performance of a Jet-Propelled Conventional and Vectored-Thrust STOL Aircraft," Journal of Aircraft, Vol. 5, No. 5, Sept.-Oct. 1968, pp. 429-436.
Kuhlman, John M., "Numerical Optimization Techniques for Bound Circulation Distribution for Minimum Induced Drag of Nonplanar Wings: Basic Formulations," NASA CR-3154, June 1979
Kuhlman, John M., and Ku, Tzuchun Jeffrey, "Numerical Optimization Techniques for Bound Circulation Distribution for Minimum Induced Drag of Nonplanar Wings: Computer Program Documentation," NASA CR-3458, Aug. 1981
Ladson, C.L., and Brooks, C.W., Jr., "Development of a Computer Program to Obtain Ordinates for NACA 6- and 6A-Series Airfoils," NASA TM X-3069, Sept., 1974.
Lamar, J.E., and Gloss, B. B. "Subsonic Aerodynamic Characteristics of Interacting Lifting Surfaces with Separated Flow around Sharp Edges Predicted by a Vortex-Lattice Method," NASA TN D-7921, Sept., 1975.
Lamar, J.E., "A Vortex Lattice Method for the Mean Camber Shapes of Trimmed Non-Coplanar Planforms with Minimum Vortex Drag," NASA TN D-8090, June, 1976.
Lamar, J.E., and Herbert, H.E., "Production Version of the Extended NASA-Langley Vortex Lattice FORTRAN Computer Code," - Volume I - User's Guide, NASA TM 83303, April 1982.
Lan, C.E., "A Quasi-Vortex-Lattice Method in Thin Wing Theory," Journal of Aircraft, Vol. 11, No. 9, September 1974, pp. 518-527.
Loftin, Laurence K., Jr., "Subsonic Aircraft: Evolution and the Matching of Size to Performance," NASA RP 1060, Aug. 1980.
Madsen, L.E., and Vanderplaats, G.N., "COPES - A FORTRAN Control Program for Engineering Synthesis," Report NPS69-81-003, Naval Postgraduate School, Monterey, CA March 1982.
Malone, B. and Mason, W.H., "Aircraft Concept Development Using Global Sensitivity Approach and Algebraic Technology Models," VPI- Aero-184, December 1991.
Malone, B. and Mason, W.H., "Aircraft Concept Optimization Using the Global Sensitivity Analysis and Parametric Multiobjective Figures of Merit," AIAA Paper 92-4221, August 1992.
Malone, B. and Mason, W.H., "Multidisciplinary Optimization in Aircraft Design Using Analytic Technology Models," Journal of Aircraft, Vol. 32, No. 2, March-April, 1995, pp. 431-438.
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.
Mason, W.H. , MacKenzie, D.A. , Stern, M.A. , Ballhaus, W.F Jr., and Frick, J., "Automated Procedure for Computing the Three-Dimensional Transonic Flow Over Wing-Body Combinations, including Viscous Effects," Vol. I, Description of Methods and Applications, Vol. II, Program User's Manual, AFFDL-TR-77-122, February 1978.
Mason, W.H., "Wing-Canard Aerodynamics at Transonic Speeds - FundamentalConsiderations on Minimum Drag Spanloads," AIAA Paper No. 82-0097, January 1982.
Mason, W.H., "Aircraft Design Information Sources," VPI-AOE-208, September 1993 (rev: February 1994). now on the web: http://www.dept.aoe.vt.edu/Mason/ACinfoTOC.html
Mason, W.H., "A Complete Engineer," Last Word, ASEE PRISM, October 1994, pg. 52
Mattingly, Jack D., Heiser, William H., and Daley, Daniel H., Aircraft Engine Design, AIAA Education Series, Washington, 1987.
Mattingly, Jack D., On-Design and Off-Design Cycle Analysis Computer Programs, AIAA, New York, 1987.
McCullers, L. A., ''Aircraft Configuration Optimization Including Optimized Flight Profiles'', NASA CP--2327, Proceedings of Symposium on Recent Experiences in Multidisciplinary Analysis and Optimization, J. Sobieski, compiler, April 1984., pp. 396-412.
Melton, John E., "EGADS: A Microcomputer Program for Estimating the Aerodynamic Performance of General Aviation Aircraft," NASA TM 104013, Jan. 1994 (N94-26091)
Nicolai, Leland M., Fundamentals of Aircraft Design, METS, Inc., 6520 Kingsland Ct., San Jose, CA 95120, 1975
Powers, S.A., "Critical Field Length Calculations for Preliminary Design," Journal of Aircraft, Vol. 18, No. 2, Feb. 1981, pp. 103-107.
Powers, Sidney A., BASIC Aircraft Performance Analysis, Kern International, Pembroke, MA, 1984
Raymer, Daniel P., Aircraft Design: A Conceptual Approach, 2nd ed., AIAA Education Series, AIAA, Washington, 1992.
Raymer, Daniel P., RDS-STUDENT: Software for Aircraft Design, Sizing, and Performance, AIAA Education Series, AIAA, Washington, 1992.
Roskam, J., Airplane Design, in eight volumes, 1985-1989, Roskam Aviation and Engineering Corporation, Ottawa, KS.
Schemensky, Roy T., "Development of an Empirically Based Computer Program to Predict the Aerodynamic Characteristics of Aircraft," Vol. I. Empirical Methods, AFFDL-TR-73-144, Nov. 1973. (AD-780 100)
Schemensky, Roy T., and Howell, George, "Aerodynamic Accounting Technique for Determining Effects of Nuclear Damage to Aircraft," Vol. I - Empirical Methods, Defense Nuclear Agency Report DNA 4531F-1, Feb. 1978 (AD A064134)
Smetana, Frederick O., Computer Assisted Analysis of Aircraft Performance Stability and Control, McGraw-Hill, New York, 1984.
Wampler, S.G., Myklebust, A., Jayaram, S., and Gelhausen, P., "Improving Aircraft Conceptual Design - A PHIGS Interactive Graphics Interface for ACSYNT," AIAA Paper 88-4481, Sept. 1988.
Williams, John E., and Vukelich, Steven P., "The USAF Stability and Control Digital DATCOM," Vol. I, User's Manual, AFFDL-TR-79-3032, April, 1979.
Vanderplaats, G.N., and Moses, F., "Structural Optimization by Methods of Feasible Directions," Computers & Structures, Vol. 3, July 1973, pp. 739-755.
Vanderplaats, G.N., "CONMIN - A FORTRAN Program for Constrained Function Minimization; User's Manual," NASA TMX-62,282, Aug. 1973.
Vanderplaats, G., "Automated Optimization Techniques for Aircraft Synthesis," AIAA Paper 76-909, Sept., 1976.