The determination of the effective resistance of a spindle supporting a model aerofoil / by W.E. Davidson and D.L. Bacon.

Format:

Book

Government document

Author/Creator:

Davidson, W. E., author.

Bacon, D. L., author.

Contributor:

United States. National Advisory Committee for Aeronautics, issuing body.

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 37.

Technical notes / National Advisory Committee for Aeronautics ; No. 37

Language:

English

Subjects (All):

Aerofoils--Testing.

Aerofoils.

Drag (Aerodynamics).

Air flow--Measurement.

Air flow.

Physical Description:

1 online resource (4 pages, 4 unnumbered pages) : illustrations

Place of Publication:

[Washington, D.C.] : National Advisory Committee for Aeronautics, 1921.

Summary:

In testing aerofoils at the Langley Memorial Aeronautical Laboratory, has determined the effective resistance of a spindle support of a model aerofoil. The largest correction applied to the values of forces observed druing model aerofoil tests is usually that necessitated by the presence of some mechanical device used to support the model in an airstream.

Notes:

Title from title screen (viewed July 1, 2019).

"January, 1921."

"Aerodynamical Laboratory, Langley Field, Va."

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical reference (page 4).

Print version record.

Other Format:

Print version: Davidson, W.E. Determination of the effective resistance of a spindle supporting a model aerofoil

OCLC:

1107323706