Investigation of distributed surface roughness on a body of revolution at a Mach number of 1.61 / K.R. Czarnecki, Ross B. Robinson, and John H. Hilton, Jr.

An investigation has been made of the effects of distributed surface roughness, consisting of lathe-tool marks, on the skin-friction drag of a body of revolution at a Mach number of 1.61. The tests were made on ogive-cylinders at zero angle of attack over a roughness range from 23 to 480 microinches...

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Bibliographic Details
Main Author: Czarnecki, K. R.
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Robinson, Ross B., Hilton, John H.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1954.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 3230.
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Call Number: Y 3.N 21/5:6/3230
Y 3.N 21/5:6/3230 Available Place a Hold