Ditching Tests of a 1/18-Scale Model of the Lockheed Constellation Airplane

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

Tests were made of a 1/18-scale dynamically similar model of the Lockheed Constellation airplane to investigate its ditching characteristics and proper ditching technique. Scale-strength bottoms were used to reproduce probable damage to the fuselage. The model was landed in calm water at the Langley tank no. 2 monorail. Various landing attitudes, speeds, and fuselage configuration were simulated. The behavior of the model was determined from visual observations, by recording the longitudinal decelerations, and by taking motion pictures of the ditchings. Data are presented in tabular form, sequence photographs, and time-history deceleration curves. It was concluded that the airplane should be ditched at a medium nose-high landing attitude with the landing flaps full down. The airplane will probably make a deep run with heavy spray and may even dive slightly. The fuselage will be damaged and leak substantially but in calm water probably will not flood rapidly. Maximum longitudinal decelerations in a calm-water ditching will be about 4g.

Authors

• Fisher, Lloyd J. National Advisory Committee for Aeronautics. Langley Aeronautical Lab.
• Morris, Garland J. National Advisory Committee for Aeronautics. Langley Aeronautical Lab.