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Spin Tests of a 1/20-Scale Model of the Bell XP-39E AirplaneIn accordance with the request of the Materiel Division, Army Air Corps, as contained in their letter to the NACA, dated August 11, 1941, tests were performed to determine the spin characteristics of a 1/20-scale model of the Bell XP-39E airplane. The effects of control dispositions were investigated, and brief tests were made with the mass distribution and center-of-gravity location varied moderately. The effect of installing an external 614-poound demolition bomb was determined, as was also the effect of modifying the tail. The results of the investigation are presented in this report.
Document ID
20150015767
Acquisition Source
Langley Research Center
Document Type
Other - NACA Memorandum Report
Authors
A I Neihouse
(Langley Memorial Aeronautical Laboratory Hampton, United States)
J W Klinar
(Langley Memorial Aeronautical Laboratory Hampton, United States)
Date Acquired
August 11, 2015
Publication Date
February 9, 1942
Publication Information
Publisher: National Advisory Committee for Aeronautics
Subject Category
Aircraft Stability and Control
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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