Formulas for use in boundary-layer calculations on low-drag wings /

Formulas for use in boundary-layer calculations on low-drag wings / by E.N. Jacobs and A.E. von Doenhoff.

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This report has been prepared in response to frequent requests received from aircraft companies for information concerning methods of computing on low-drag the (1) Transition point, (2) Velocity distribution in laminar and turbulent boundary layers, (3) Thickness of the boundary layer, both laminar...

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Bibliographic Details
Main Author: Jacobs, Eastman N. (Eastman Nixon), 1902-1987
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Von Doenhoff, Albert E.
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1941]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L319.
Subjects:
Aerofoils.
Boundary layer.
Mathematics > Formulae.
Mathematics.
Mathematical formulae.

Norlin Library - Basement - Government Information - US

Holdings details from Norlin Library - Basement - Government Information - US
Call Number: Y 3.N 21/5:11/L319
Y 3.N 21/5:11/L319 Available Place a Hold

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