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Propeller design. IV, A simple method for determining the strength of propellers

Author: Fred E Weick; United States. National Advisory Committee for Aeronautics,
Publisher: [Washington, D.C.] : National Advisory Committee for Aeronautics, 1926.
Series: Technical note (United States. National Advisory Committee for Aeronautics), 238.
Edition/Format:   eBook : Document : National government publication : EnglishView all editions and formats
Summary:
The object of this report, the last of a series of four on propeller design, is to describe a simple method for determining whether the strength of a propeller of a standard form is sufficient for safe operation. An approximate method of stress analysis is also given.
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Additional Physical Format: Print version:
Weick, Fred E.
Propeller design : a simple method for determining the strength of propellers. IV
(OCoLC)642055809
Material Type: Document, Government publication, National government publication, Internet resource
Document Type: Internet Resource, Computer File
All Authors / Contributors: Fred E Weick; United States. National Advisory Committee for Aeronautics,
OCLC Number: 1127388904
Notes: "June 1926."
"Langley Memorial Aeronautical Laboratory."
No Federal Depository Library Program (FDLP) item number.
Reproduction Notes: Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.
Description: 1 online resource (11 pages, 5 unnumbered pages) : illustrations.
Details: Master and use copy. Digital master created according to Technical Guidelines for Digitizing Archival Materials for Electronic Access. U.S. National Archives and Records Administration, 2004.
Series Title: Technical note (United States. National Advisory Committee for Aeronautics), 238.
Other Titles: Simple method for determining the strength of propellers
Responsibility: by Fred E. Weick.

Abstract:

The object of this report, the last of a series of four on propeller design, is to describe a simple method for determining whether the strength of a propeller of a standard form is sufficient for safe operation. An approximate method of stress analysis is also given.

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