Effect Of Horizontal Tail Location On Low Speed Static Longitudinal Stability And Damping In Pitch Of A Model Having 45 Sweptback Wing And Tail Surfaces

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Effect of Horizontal-tail Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces

Effect of Horizontal-tail Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces
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Total Pages : 34
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ISBN-10 : UOM:39015086495507
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Book Synopsis Effect of Horizontal-tail Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces by : Jacob H. Lichtenstein

Download or read book Effect of Horizontal-tail Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces written by Jacob H. Lichtenstein and published by . This book was released on 1951 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind-tunnel results are presented to show the effect of changes in horizontal-tail location on the low-speed static longitudinal stability and steady-state rotary damping in pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees.


Effect of Horizontal-tail Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces Related Books

Effect of Horizontal-tail Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces
Language: en
Pages: 34
Authors: Jacob H. Lichtenstein
Categories: Airplanes
Type: BOOK - Published: 1951 - Publisher:

DOWNLOAD EBOOK

Wind-tunnel results are presented to show the effect of changes in horizontal-tail location on the low-speed static longitudinal stability and steady-state rota
Effect of Horizontal-tail Size and Tail Length on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces
Language: en
Pages: 40
Authors: Jacob H. Lichtenstein
Categories: Airplanes
Type: BOOK - Published: 1951 - Publisher:

DOWNLOAD EBOOK

Wind-tunnel results of the effects of horizontal-tail size and length on the low-speed static longitudinal stability and the steady-state rotary damping in pitc
Effect of Horizontal-tail Size and Tail Length on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Degrees Sweptback Wing and Tail Surfaces
Language: en
Pages: 32
Authors: Jacob H. Lichtenstein
Categories: Airplanes
Type: BOOK - Published: 1951 - Publisher:

DOWNLOAD EBOOK

Wind-tunnel results of the effects of horizontal-tail size and length on the low-speed static longitudinal stability and the steady-state rotary damping in pitc