Loads and calculations of Army airplanes / by Ing. Stelmachowski.

Format:

Book

Government document

Author/Creator:

Stelmachowski, Ing., author.

Contributor:

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

Series:

Technical note (United States. National Advisory Committee for Aeronautics) ; 28.

Technical notes / National Advisory Committee for Aeronautics ; No. 28

Language:

English

Subjects (All):

Airplanes.

Loads (Mechanics)--Mathematical models.

Loads (Mechanics).

airplanes.

Physical Description:

1 online resource (11 pages) : illustrations

Place of Publication:

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

Summary:

A military airplane must fulfill two conditions: (1) it must be aerodynamically capable of good performance, and (2) it must also be structurally strong enough to maneuver without risk of failure. Based on experience and scientific investigations, standards have been developed which are satisfactory for the calculation of airplane structures.

Notes:

Title from title screen (viewed June 20, 2019).

"February, 1921."

"Translated from Technische Berichte, Vol. III, Section 6, by the Office of Naval Intelligence, U.S.N."

[Written by Ing. Stelmachowski ... "Ing" is most likely short for "Engineer"].

No Federal Depository Library Program (FDLP) item number.

Includes bibliographical references (page 8).

Print version record.

Other Format:

Print version: Stelmachowski, Ing. Loads and calculations of Army airplanes

OCLC:

1105632565