The Effects of Fuel Sloshing on the Lateral Stability of a Free-Flying Airplane Model Page: 18 of 36
35 p. : ill.View a full description of this report.
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NACA RM No. L8016
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DepA of water nthe tanks, inches
Figure 4.- Variation of mass ratio with depth of water in tanks.
17
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Smith, Charles C., Jr. The Effects of Fuel Sloshing on the Lateral Stability of a Free-Flying Airplane Model, report, June 29, 1948; (https://digital.library.unt.edu/ark:/67531/metadc57576/m1/18/: accessed April 24, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.