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Drag of C-Class Airship Hulls of Various Fineness RatiosThis report presents the results of wind-tunnel tests on eight C-class airship hulls with various fineness ratios, conducted in the Navy Aerodynamic Laboratory, Washington. The purpose of the tests was to determine the variation of resistance with fineness ratio, and also to find the pressure and friction elements of the total drag for the model having the least shape coefficient. Seven C-class airship hulls with fineness ratios of 1.0, 1.5, 2.0, 3.0, 6.0, 8.0, and 10.0 were made and verified. These models and also the previously constructed original C-class hull, whose fineness ratio is 4.62, were then tested in the 8 by 8 foot tunnel for drag of 0 degree pitch and yaw, at various wind speeds. The original hull, which was found to have the least shape coefficient, was then tested for pressure distribution over the surface at various wind speeds. (author)
Document ID
19930091360
Document Type
Other
Authors
Zahm, A F
Smith, R H
Louden, F A
Date Acquired
September 6, 2013
Publication Date
January 1, 1929
Report/Patent Number
NACA-TR-291
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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