Analysis of Dr. Schaffran's propeller model tests / by Max M. Munk.

Format:

Book

Government document

Author/Creator:

Munk, Max M. (Max Michael), 1890- author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 158.

Technical notes / National Advisory Committee for Aeronautics ; No. 158

Language:

English

Subjects (All):

Propellers, Aerial--Models.

Propellers, Aerial.

Propellers, Aerial--Testing.

Physical Description:

1 online resource (5 pages, 8 unnumbered pages) : illustrations.

Place of Publication:

[Washington, D.C.] : National Advisory Committee for Aeronautics, 1923.

Summary:

This technical note, prepared for the National Advisory Committee for Aeronautics, contains an analysis of the propeller model tests of Dr. Schaffran. This analysis was made in the same was as that of Dr. Durand's tests. Only the thrust is examined. It appears that the thrust produced by three blade and four-blade propellers follows the same laws as with two-blade propellers, and that all conclusions reached from Dr. Durand's tests can be upheld.

Notes:

Title from title screen (viewed August 9, 2019).

"September 1923."

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical reference (page 1).

Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.

Other Format:

Print version: Munk, Max M. Analysis of Dr. Schaffran's propeller model tests

OCLC:

1117765923