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Tabulated Pressure Coefficient Data from a Tail Loads Investigation on a 1/15-Scale Model of the Goodyear XZP5K AirshipThis paper contains tail and hull loads data obtained in an investigation of a l/15-scale model of the Goodyear XZP5K airship. Data are presented in the form of tabulated pressure coefficients over a pitch and yaw range of +/-20 deg and 0 deg to 30 deg respectively, with various rudder and elevator deflections. Two tail configurations of different plan forms were tested on the model. The investigation was conducted in the Langley full-scale tunnel at a Reynolds number of approximately 16.5 x 10(exp 6) based on hull length, which corresponds to a Mach number of about 0.12.
Document ID
20050028484
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Cannon, Michael D. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 22, 2013
Publication Date
January 1, 1956
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-RM-SL56C12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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