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
Title 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 PDF eBook
Author Jacob H. Lichtenstein
Publisher
Pages 34
Release 1951
Genre Airplanes
ISBN

Download 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 Book in PDF, Epub and Kindle

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 Size and Tail Length on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces

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
Title 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 PDF eBook
Author Jacob H. Lichtenstein
Publisher
Pages 40
Release 1951
Genre Airplanes
ISBN

Download 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 Book in PDF, Epub and Kindle

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 pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees and aspect ratios of 4 are presented.

Effect of Horizontal-tail Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Degrees 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 Degrees Sweptback Wing and Tail Surfaces
Title Effect of Horizontal-tail Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Degrees Sweptback Wing and Tail Surfaces PDF eBook
Author
Publisher
Pages
Release 1951
Genre
ISBN

Download Effect of Horizontal-tail Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Degrees Sweptback Wing and Tail Surfaces Book in PDF, Epub and Kindle

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

Effect of Horizontal-tail Size and Tail-length on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Degree Sweptback Wing and Tail Surfaces
Title Effect of Horizontal-tail Size and Tail-length on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Degree Sweptback Wing and Tail Surfaces PDF eBook
Author Jacob H. Lichtenstein
Publisher
Pages
Release 1951
Genre
ISBN

Download Effect of Horizontal-tail Size and Tail-length on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 Degree Sweptback Wing and Tail Surfaces Book in PDF, Epub and Kindle

Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces

Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces
Title Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces PDF eBook
Author Arthur Earl Bryson
Publisher
Pages 340
Release 1952
Genre Aeronautics
ISBN

Download Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces Book in PDF, Epub and Kindle

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

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
Title 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 PDF eBook
Author Jacob H. Lichtenstein
Publisher
Pages 32
Release 1951
Genre Airplanes
ISBN

Download 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 Book in PDF, Epub and Kindle

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 pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees and aspect ratios of 4 are presented.

Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics
Title Technical Note - National Advisory Committee for Aeronautics PDF eBook
Author United States. National Advisory Committee for Aeronautics
Publisher
Pages 1146
Release 1957
Genre Aeronautics
ISBN

Download Technical Note - National Advisory Committee for Aeronautics Book in PDF, Epub and Kindle