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A method for calculating the pressure distribution over jet-flapped wings / by D. Küchemann.

The incompressible flow past an aerofoil with a thin jet emerging from its lower surface somewhere near the trailing edge is considered. A simple method is described for calculating the pressure distribution over wings of non-zero thickness. The possible effects of sweep are briefly discussed. It...

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Bibliographic Details
Main Author: Küchemann, Dietrich, 1911-1976
Corporate Authors: Aeronautical Research Council (Great Britain), Royal Aircraft Establishment (Great Britain)
Format: Book
Language:English
Published: London : H.M.S.O, 1957.
Series:Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3036.
Subjects:
Aerodynamic load > Mathematical models.
Aerofoils > Aerodynamics.
Incompressible flow.
Jet flaps (Airplanes) > Aerodynamics > Mathematical models.

Norlin Library - Basement - Government Information - Foreign

Holdings details from Norlin Library - Basement - Government Information - Foreign
Call Number: 301-Ae8 4:
301-Ae8 4: (3026-3049 1953-57) Available Place a Hold

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