The effect of T-tail empennage geometry on the directional and lateral stability derivatives

dc.contributor.advisorWierum, Frederic A.en_US
dc.creatorHoward, Roland M.en_US
dc.date.accessioned2018-12-18T21:28:48Zen_US
dc.date.available2018-12-18T21:28:48Zen_US
dc.date.issued1977en_US
dc.description.abstractThe advent of the utilization of the T-tail in light aircraft design requires that new consideration be given as to the effect of imposed loads on the empennage and on the stability derivatives, each of which is greatly influenced. This thesis presents the results of wind tunnel tests of a model consisting of a fuselage, a vertical fin, and a horizontal stabilizer. Five different horizontal stabilizers (T-tails), each with a different aspect ratio and longitudinal position were tested. Theoretical calculations are compared with the test results, and discussion given as to the optimization of these geometric parameters.en_US
dc.format.digitalOriginreformatted digitalen_US
dc.format.extent65 ppen_US
dc.identifier.callnoTHESIS M.E. 1977 HOWARDen_US
dc.identifier.citationHoward, Roland M.. "The effect of T-tail empennage geometry on the directional and lateral stability derivatives." (1977) Master’s Thesis, Rice University. <a href="https://hdl.handle.net/1911/104694">https://hdl.handle.net/1911/104694</a>.en_US
dc.identifier.digitalRICE2330en_US
dc.identifier.urihttps://hdl.handle.net/1911/104694en_US
dc.language.isoengen_US
dc.rightsCopyright is held by the author, unless otherwise indicated. Permission to reuse, publish, or reproduce the work beyond the bounds of fair use or other exemptions to copyright law must be obtained from the copyright holder.en_US
dc.titleThe effect of T-tail empennage geometry on the directional and lateral stability derivativesen_US
dc.typeThesisen_US
dc.type.materialTexten_US
thesis.degree.departmentMechanical Engineeringen_US
thesis.degree.disciplineEngineeringen_US
thesis.degree.grantorRice Universityen_US
thesis.degree.levelMastersen_US
thesis.degree.nameMaster of Scienceen_US
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