Abstract
1 Luskin, L. and Lapin, E., An Analytical Approach to the Fuel Sloshing and Buffeting Problems of Aircraft, J. Aeronaut. Sci., vol. 19, no. 4, April 1952, pp. 217-228. 2 Graham, E. W. and Rodriquez, A. M., The Characteristics of Fuel Motion Which Affect Airplane Dynamics, J. Appl. Mech., vol. 19, no. 3, September 1952, pp. 381-388 (see also Douglas Aircraft Co. Rep. No. SM-14212). 3 Kachigan, K., Forced Oscillations of a in a Cylindrical Tank, Convair Rep. ZU-7-046, October 1955. 4 Schmitt, A. F., Forced Oscillations of a in a Cylindrical Tank Undergoing Translation and Rotation, Convair Rep. ZU-7-069, October 1956. 5 Bauer, H. F., Pluid Oscillations in a Circular Cylindrical Tank, ABM A Rep. DA-TR-1-58, April 1958. 6 Bauer, H. F., Fluid Oscillations in a Cylindrical Tank With Damping, ABM A Rep. DA-TR-4-58, April 1958. 7 Miles, J. W., On the Sloshing of in a Cylindrical Tank, Ramo-Wooldridge Rep. AM6-5, April 1956. 8 Bauer, H. F., The Moment of Inertia of a in a Circular Cylindrical Tank, ACM A DA-TR-5-58, April 1958. 9 Chu, W. H., Free Surface Condition for Sloshing Resulting From Pitching and Some Corrections, ARS JOURNAL, vol. 30, no. 11, November I960, pp. 1093-1094. 10 Abramson, H. N. and Ransleben, G. E., Jr., Simulation of Fuel Sloshing Characteristics in Missile Tanks by Use of Small Models, ARS JOURNAL, vol. 30, no. 7, July 1960, pp. 603-612. 11 Abramson, H. N. and Ransleben, G. E., Jr., Liquid Sloshing in Rigid Cylindrical Tanks Undergoing Pitching Motion, Tech. Rep. no. 11, Contract no. DA 23-072-ORD-1251, Southwest Research Inst . , May 1961.
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