The effect of longitudinal moment of inertia upon dynamic stability /

The effect of longitudinal moment of inertia upon dynamic stability /

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Bibliographic Details
Author / Creator:Norton, F. H. (Frederick Harwood), 1896-1992, author.
Imprint:[Washington, D.C.] : National Advisory Committee for Aeronautics, 1922.
Description:1 online resource (3 pages, 1 unnumbered page) : illustration.
Language:English
Series:Technical notes / National Advisory Committee for Aeronautics ; No. 115
Technical note (United States. National Advisory Committee for Aeronautics) ; 115.
Subject:
Stability of airplanes.
Stability of airplanes, Longitudinal.
Moments of inertia.
Moments of inertia.
Stability of airplanes.
Stability of airplanes, Longitudinal.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/12092491
Hidden Bibliographic Details
Other authors / contributors:Carroll, Thomas, author.
United States. National Advisory Committee for Aeronautics, issuing body.
Notes:"October, 1922."
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical reference (page 1).
Description based on online resource, PDF version; title from title page (TRAIL, viewed March 25, 2020).
Other form:Print version: Norton, F. H. Effect of longitudinal moment of inertia upon dynamic stability
GPO item no.:9999 (online)
Govt.docs classification:Y 3.N 21/5:6/115

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