Effects of Horizontal-tail Position, Area, and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degrees Triangular-wing Model Having Various Triangular-all-movable Horizontal Tails PDF Download

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Effects of Horizontal-tail Position, Area, and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degrees Triangular-wing Model Having Various Triangular-all-movable Horizontal Tails

Effects of Horizontal-tail Position, Area, and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degrees Triangular-wing Model Having Various Triangular-all-movable Horizontal Tails PDF Author: Byron M. Jaquet
Publisher:
ISBN:
Category :
Languages : en
Pages : 61

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Book Description

Effects of Horizontal-tail Position, Area, and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degrees Triangular-wing Model Having Various Triangular-all-movable Horizontal Tails

Effects of Horizontal-tail Position, Area, and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degrees Triangular-wing Model Having Various Triangular-all-movable Horizontal Tails PDF Author: Byron M. Jaquet
Publisher:
ISBN:
Category :
Languages : en
Pages : 61

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Book Description

Effects of Horizontal-tail Position and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degree Triangular-wing Model Having Twin Triangular All-movable Tails

Effects of Horizontal-tail Position and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degree Triangular-wing Model Having Twin Triangular All-movable Tails PDF Author: Byron M. Jaquet
Publisher:
ISBN:
Category :
Languages : en
Pages : 45

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Book Description

Low-speed Static Lateral Stability Characteristics of a Canard Model Having a 60© Triangular Wing and Horizontal Tail

Low-speed Static Lateral Stability Characteristics of a Canard Model Having a 60© Triangular Wing and Horizontal Tail PDF Author: William R. Bates
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 38

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Book Description

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 PDF Author: Jacob H. Lichtenstein
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34

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Book Description
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 PDF Author: Jacob H. Lichtenstein
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40

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Book Description
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.

An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability Below the Mach Number of Lift Divergence

An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability Below the Mach Number of Lift Divergence PDF Author: John A. Axelson
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 20

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Book Description
An analysis is presented of the influence of wing aspect ratio and tail location on the effects of compressibility upon static longitudinal stability. The investigation showed that the use of reduced wing aspect ratios or short tail lengths leads to serious reductions in high-speed stability and the possibility of high-speed instability.

Summary and Analysis of Horizontal-tail Contribution to Longitudinal Stability of Swept-wing Airplanes at Low Speeds

Summary and Analysis of Horizontal-tail Contribution to Longitudinal Stability of Swept-wing Airplanes at Low Speeds PDF Author: Robert H. Neely
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 100

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Book Description
Air-flow characteristics behind wings and wing-body combinations are described and are related to the downwash at specific tail locations for unseparated and separated flow conditions. The effects of various parameters and control devices on the air-flow characteristics and tail contribution are analyzed and demonstrated. An attempt has been made to summarize certain data in a form useful for design. The experimental data herein were obtained mostly at Reynolds numbers greater than 4 x 105 and at Mach numbers less than 0.25.

Israel Journal of Technology

Israel Journal of Technology PDF Author:
Publisher:
ISBN:
Category : Engineering
Languages : en
Pages : 376

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Book Description
Includes proceedings of various meetings and conferences.

Effects of Wing and Tail Location on the Aerodynamic Characteristics of an Airplane for Mach Numbers from 0.25 to 4.63

Effects of Wing and Tail Location on the Aerodynamic Characteristics of an Airplane for Mach Numbers from 0.25 to 4.63 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Book Description

Effects of Wing Position and Horizontal-tail Position on the Static Stability Characteristics of Models with Unswept and 45 Degrees Sweptback Surfaces with Some Reference to Mutual Interference

Effects of Wing Position and Horizontal-tail Position on the Static Stability Characteristics of Models with Unswept and 45 Degrees Sweptback Surfaces with Some Reference to Mutual Interference PDF Author: Alex Goodman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 58

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Book Description
Results are presented of an investigation made to determine the effects of wing position and horizontal-tail position on the low-speed static static lateral and static longitudinal stability characteristics of airplane models having unswept and 45 degree sweptback surfaces. Interference increments between the various components are evaluated, and efficiency factors of the vertical tail as a function of wing position are presented.