Effect of Vertical-tail Area and Length on the Yawing Stability Characteristics of a Model Having a 45° Sweptback Wing PDF Download

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Effect of Vertical-tail Area and Length on the Yawing Stability Characteristics of a Model Having a 45° Sweptback Wing

Effect of Vertical-tail Area and Length on the Yawing Stability Characteristics of a Model Having a 45° Sweptback Wing PDF Author: William Letko
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 58

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Book Description
Contains wind-tunnel results of an investigation made in the Langley stability tunnel to determine the effects of vertical-tail area and length on the low-speed yawing derivatives of a midwing airplane model having a 45 degree sweptback wing and tail surfaces. Comparisons of the measured contributions with those calculated by currently available procedures are also presented. The interference between the various model components is discussed.