Flight Measurements to Determine Effect of a Spring-Loaded Tab on Longitudinal Stability of an Airplane Page: 1 of 41
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ARR No. L5120
NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS
WA IT I I E /POIT
February 1946 as
Advance Restricted Report L5120
FLIGHT MEASUREMENTS TO DETERMINE EFFECT OF A SPRING-LOADED
TAB ON LONGITUDINAL STABILITY OF AN AIRPLANE
By Paul A. Hunter and John P. Reeder
Langley Memorial Aeronautical Laboratory
Langley Field, Va.
NACA WARTIME REPORTS are reprints of papers originally issued to provide rapid distribution of
advance research results to an authorized group requiring them for the war effort. They were pre-
tiously held under a security status but are now unclassified. Some of these reports were not tech-
nically edited. All have been reproduced without change in order to expedite general distribution.
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Hunter, Paul A. & Reeder, John P. Flight Measurements to Determine Effect of a Spring-Loaded Tab on Longitudinal Stability of an Airplane, report, February 1, 1946; (digital.library.unt.edu/ark:/67531/metadc60957/m1/1/: accessed September 22, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.