Low-speed Investigation of the Effects of Wing Dihedral Angle and Fin Length on the Static Stability Characteristics of a Model Having an 82 Degree Delta Wing PDF Download

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Low-speed Investigation of the Effects of Wing Dihedral Angle and Fin Length on the Static Stability Characteristics of a Model Having an 82 Degree Delta Wing

Low-speed Investigation of the Effects of Wing Dihedral Angle and Fin Length on the Static Stability Characteristics of a Model Having an 82 Degree Delta Wing PDF Author: Kenneth P. Spreemann
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

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Book Description

Low-speed Investigation of the Effects of Wing Dihedral Angle and Fin Length on the Static Stability Characteristics of a Model Having an 82 Degree Delta Wing

Low-speed Investigation of the Effects of Wing Dihedral Angle and Fin Length on the Static Stability Characteristics of a Model Having an 82 Degree Delta Wing PDF Author: Kenneth P. Spreemann
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

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Book Description

Effects of Wing Position and Fuselage Size on the Low-speed Static and Rolling Stability Characteristics of a Delta-wing Model

Effects of Wing Position and Fuselage Size on the Low-speed Static and Rolling Stability Characteristics of a Delta-wing Model PDF Author: Alex Goodman
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 82

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Book Description
An investigation was made to determine the effects of wing position and fuselage size on the low-speed static and rolling stability characterististics of airplane models having a triangular wing and vertical tail surfaces.

Low-speed Investigation of the Effects of Frequency and Amplitude of Oscillation in Sideslip on the Lateral Stability Derivatives of a 60 Degree Delta Wing, a 40 Degree Sweptback Wing and an Unswept Wing

Low-speed Investigation of the Effects of Frequency and Amplitude of Oscillation in Sideslip on the Lateral Stability Derivatives of a 60 Degree Delta Wing, a 40 Degree Sweptback Wing and an Unswept Wing PDF Author: Jacob H. Lichtenstein
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

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Book Description

Low-speed Measurements of Static Stability, Damping in Yaw, and Damping in Roll of a Delta, a Swept, and an Unswept Wing for Angles of Attack from 0 Degrees to 90 Degrees

Low-speed Measurements of Static Stability, Damping in Yaw, and Damping in Roll of a Delta, a Swept, and an Unswept Wing for Angles of Attack from 0 Degrees to 90 Degrees PDF Author: Joseph L. Johnson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 19

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Book Description
A low-speed investigation has been conducted to determine the static longitudinal and lateral stability characteristics and the damping in yaw and damping in roll of a 60 degree delta wing, a 45 degree swept wing of aspect ratio 2.61, and an unswept wing of aspect ratio 3 over an angle-of-attack range from 0 to 90 degrees.

Aeronautical Engineering Index

Aeronautical Engineering Index PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1212

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Book Description

Aerospace Engineering Index

Aerospace Engineering Index PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 292

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Book Description

Effect of Geometric Dihedral on Low-speed Static Stability Characteristics of a 40 Degree Swept-back Wing

Effect of Geometric Dihedral on Low-speed Static Stability Characteristics of a 40 Degree Swept-back Wing PDF Author: Kazimierz Orlik-Ruckemann
Publisher:
ISBN:
Category :
Languages : en
Pages : 18

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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

Investigation of Effects of Geometric Dihedral on Low-speed Static Stability and Yawing Characteristics of an Untapered 45° Sweptback-wing Model of Aspect Ratio 2.61

Investigation of Effects of Geometric Dihedral on Low-speed Static Stability and Yawing Characteristics of an Untapered 45° Sweptback-wing Model of Aspect Ratio 2.61 PDF Author: M. J. Queijo
Publisher:
ISBN:
Category :
Languages : en
Pages : 29

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Book Description

Stability and Control Characteristics at Low Speed of an Airplane Model Having a 38.7 Degree Sweptback Wing with Aspect Ratio 4.51, Taper Ratio 0.54, and Conventional Tail Surfaces

Stability and Control Characteristics at Low Speed of an Airplane Model Having a 38.7 Degree Sweptback Wing with Aspect Ratio 4.51, Taper Ratio 0.54, and Conventional Tail Surfaces PDF Author: Vernard E. Lockwood
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 155

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Book Description
Contains the results of a low-speed wind-tunnel investigation to determine the static stability and control characteristics of an airplane model having a leading-edge sweep of 38.7 degrees, aspect ratio of 4.51, and a taper ratio of 0.54. In addition to the complete model investigation the effects of leading edges slots, a circular-arc wing, drooped leading edges, change of tail length, and change of fin area on the aerodynamic characteristics were determined. Also includes an analysis of wing-fuselage interference effect on effective dihedral.