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Langley Field wind tunnel apparatus. Part I, Regulators for speed of wind tunnel drive motor. Part II, A Vernier manometer with adjustable sensitivity / by D.L. Bacon.

U.S. Government Documents Available online

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Format:
Book
Government document
Author/Creator:
Bacon, D. L., author.
Contributor:
United States. National Advisory Committee for Aeronautics, issuing body.
Series:
Technical note (United States. National Advisory Committee for Aeronautics) ; 81.
Technical notes / National Advisory Committee for Aeronautics ; No. 81
Language:
English
Subjects (All):
Wind tunnels--Testing.
Wind tunnels.
Physical Description:
1 online resource (9 pages, 2 unnumbered pages) : illustrations.
Place of Publication:
[Washington, D.C.] : National Advisory Committee for Aeronautics, 1922.
Summary:
This report explores two aspects of the instrumentation of the Langley Field wind tunnel and associated apparatus.
Contents:
Part I. Regulators for speed of wind tunnel drive motor
Part II. A Vernier manometer with adjustable sensitivity.
Notes:
Title from title screen (viewed July 1, 2019).
"January, 1922."
"Langley Memorial Aeronautical Laboratory, National Advisory Committee for Aeronautics, Langley Field, Va."
No Federal Depository Library Program (FDLP) item number.
Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.
Other Format:
Print version: Bacon, D. L. Langley Field wind tunnel apparatus
OCLC:
1107323823

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