G.D. McCann and R.H. MacNeal, Beam Vibration Analysis with an Electric-Analog Computer, J. Appl. Mech ., vol. 72, pp. 13-26; March, 1950.
2.
R.H. MacNeal , The Solution of Elastic Plate Problems by Electric Analogies, J. Appl. Mech., vol. 18, pp. 59-67; March, 1951.
3.
S.V. Benscoter and R.H. MacNeal, Equivalent Plate Theory for a Straight Multicell Wing , NACA Tech. Note 2786; September, 1952.
4.
S.V. Benscoter and R.H. MacNeal, Analysis of Straight Multicell Wings on Cal-Tech Analog Computer, NACA Tech Note 3113; January, 1954.
5.
R.H. MacNeal and S.V. Benscoter, Analysis of Multicell Delta Wings on Cal-Tech Analog Computer, NACA Tech. Note 3114; December, 1953.
6.
R.H. MacNeal and S.V. Benscoter, Analysis of Sweptback Wings on Cal-Tech Analog Computer, NACA Tech. Note 3115; January, 1954 .
7.
C.E. Howe, R.M. Howe, and L.L. Rauch, Engrg. Res. Inst., Univ. of Michigan, Ann Arbor, Memo. UMN-67; January 1951.
8.
See also, R.M. Howe and V.S. Haneman, Jr., The Solution of Partial Differential Equations by Difference Methods Using the Electronic Differential Analyzer, Proc. IRE, vol. 41, pp. 1497-1508; October, 1953.
9.
Simulation Council Newsletter, Instr. and Automation , vol. 30, pp. 1515-1520; August, 1957.
10.
M. Yanowitch , Solution of a Flutter Problem, Project Cyclone Rept.; June, 1955.
11.
F.B. Hildebrand , Introduction to Numerical Analysis , McGraw-Hill Book Co., Inc., New York, N. Y., p. 439; 1956.
12.
V.L. Larrowe , Direct Simulation Bypasses Mathematics, Simplifies Analysis, Control Engrg., vol. 1, p. 25 ff; November, 1954.
13.
A. Karen and B.D. Loveman, Large Problem Solutions at Project Cyclone, Instr. and Automation , vol. 29, pp. 78-83; January, 1956.
14.
S. Timoshenko , Theory of Plates and Shells, McGraw-Hill Book Co., Inc., New York, N. Y., ch. 4; 1940.
15.
D. Williams and P.C. Birschall, Solution of the Problem of the Cantilever Square Plate by the Use of Influence Coefficients and a High Speed Digital Computer, Royal Aircraft Estab., Farnborough, Hants, Eng., Tech. Note Structures 178; 1956.