An Evaluation of an Accelerometer Method for Obtaining Landing-Gear Drag Loads Page: 1 of 25
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zNATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS
TECHNICAL NOTE 3247
AN EVALUATION OF AN ACCELEROMETER METHOD FOR
OBTAINING LANDING-GEAR DRAG LOADS
By Jerome G. Theisen and Philip M. Edge, Jr.
Langley Aeronautical Laboratory
Langley Field, Va.
NACA
Washington
October 1954Li
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Theisen, Jerome G. & Edge, Philip M., Jr. An Evaluation of an Accelerometer Method for Obtaining Landing-Gear Drag Loads, report, October 1954; (https://digital.library.unt.edu/ark:/67531/metadc57140/m1/1/: accessed April 25, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.