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 |
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
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 |
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
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 |
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 |
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 |
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 |
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
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 |