Notes on propeller design. III, The aerodynamical equations of the propeller blade elements / 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) ; 95.

Technical notes / National Advisory Committee for Aeronautics ; No. 95

Language:

English

Subjects (All):

Propellers, Aerial.

Propellers, Aerial--Design and construction.

Air flow.

Physical Description:

1 online resource (10 pages) : illustration.

Place of Publication:

[Washington D.C.] : National Advisory Committee for Aeronautics, 1922.

Summary:

The air flow and the air force created by all elements of the propeller blades lying in a ring located between two concentric circles around the propeller axis are independent of what happens in other rings. The aerodynamic equations of such blade elements are setablished and their application is discussed.

Notes:

Title from title screen (viewed August 5 2019).

"May, 1922."

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: Munk, Max M. (Max Michael), 1890- Notes on propeller design - 3.

OCLC:

1111581289