Effects of the Spanwise, Chordwise, and Vertical Location of an External Store on the Aerodynamic Characteristics of a 45 Degree Sweptback Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96 PDF Download

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Effects of the Spanwise, Chordwise, and Vertical Location of an External Store on the Aerodynamic Characteristics of a 45 Degree Sweptback Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96

Effects of the Spanwise, Chordwise, and Vertical Location of an External Store on the Aerodynamic Characteristics of a 45 Degree Sweptback Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96 PDF Author: Carl R. Jacobsen
Publisher:
ISBN:
Category :
Languages : en
Pages : 31

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Book Description

Effects of the Spanwise, Chordwise, and Vertical Location of an External Store on the Aerodynamic Characteristics of a 45 Degree Sweptback Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96

Effects of the Spanwise, Chordwise, and Vertical Location of an External Store on the Aerodynamic Characteristics of a 45 Degree Sweptback Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96 PDF Author: Carl R. Jacobsen
Publisher:
ISBN:
Category :
Languages : en
Pages : 31

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Book Description

Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45© Sweptback Wing of Aspect Ratio 4 and a 60© Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96

Effects of Size of External Stores on the Aerodynamic Characteristics of an Unswept and a 45© Sweptback Wing of Aspect Ratio 4 and a 60© Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96 PDF Author: Carl R. Jacobsen
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62

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Book Description

Effects of Systematically Varying the Spanwise and Vertical Location of an External Store on the Aerodynamic Characteristics of an Unswept Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96

Effects of Systematically Varying the Spanwise and Vertical Location of an External Store on the Aerodynamic Characteristics of an Unswept Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96 PDF Author: Carl R. Jacobsen
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Book Description

Effects of the Spanwise, Chordwise, and Vertical Location of an External Store on the Aerodynamic Characteristics of a 60 Degree Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96

Effects of the Spanwise, Chordwise, and Vertical Location of an External Store on the Aerodynamic Characteristics of a 60 Degree Delta Wing at Mach Numbers of 1.41, 1.62, and 1.96 PDF Author: Carl R. Jacobsen
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Book Description

Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61

Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61 PDF Author: Emma Jean Landrum
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 70

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Book Description

Aerodynamic Loading Characteristics in Sideslip of a 45© Sweptback Wing with and Without a Fence at High Subsonic Speeds

Aerodynamic Loading Characteristics in Sideslip of a 45© Sweptback Wing with and Without a Fence at High Subsonic Speeds PDF Author: Richard E. Kuhn
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 50

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Book Description

Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45© Swept-back Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 106 to 4.8 X 10 as Determined by Pressure Distributions, Force Tests, and Calculations

Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45© Swept-back Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 106 to 4.8 X 10 as Determined by Pressure Distributions, Force Tests, and Calculations PDF Author: George L. Pratt
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 110

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Book Description

Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45© Sweptback Wing at High Subsonic Speeds

Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45© Sweptback Wing at High Subsonic Speeds PDF Author: James W. Wiggins
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 32

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Book Description

Effects of Spanwise Thickness Variation on the Aerodynamic Characteristics of 35 Degree and 45 Degree Sweptback Wings of Aspect Ratio 6

Effects of Spanwise Thickness Variation on the Aerodynamic Characteristics of 35 Degree and 45 Degree Sweptback Wings of Aspect Ratio 6 PDF Author: William D. Morrison
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38

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Book Description
An aerodynamic investigation has been conducted in the Langley high-speed 7- by 10-foot tunnel to determine the effects of taper-in-thickness on the aerodynamics characteristics of wings having 35 and 45 degrees of sweep-back, aspect ratio 6, and taper ratio 0.60. The wings were tapered from NACA 65A009 airfoil sections at the root chord to NACA 65A003 airfoil sections at the tip chord. The test Mach number range was from 0.60 to 1.14 at a Reynolds number of the order of 500,000.

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.