Wind-tunnel Investigation of the Aerodynamic Characteristics in Pitch and Sideslip at High Subsonic Speeds of a Wing-fuselage Combination Having a Triangular Wing of Aspect Ratio 4

Wind-tunnel Investigation of the Aerodynamic Characteristics in Pitch and Sideslip at High Subsonic Speeds of a Wing-fuselage Combination Having a Triangular Wing of Aspect Ratio 4
Author: Paul G. Fournier
Publisher:
Total Pages: 34
Release: 1953
Genre: Airplanes
ISBN:
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The results presented in the present paper are part of a program conducted to investigate the effect of wing plan form on the aerodynamic characteristics in pitch, in sideslip, and during steady roll. This paper presents the aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a wing-fuselage combination having a triangular wing of aspect ratio 4, a leading-edge sweep of angle of 45 degrees, and with an NACA 65A006 airfoil section parallel to the plane of symmetry.


Wind-tunnel Investigation of the Aerodynamic Characteristics in Pitch and Sideslip at High Subsonic Speeds of a Wing-fuselage Combination Having a Triangular Wing of Aspect Ratio 4
Language: en
Pages: 34

Wind-tunnel Investigation of the Aerodynamic Characteristics in Pitch and Sideslip at High Subsonic Speeds of a Wing-fuselage Combination Having a Triangular Wing of Aspect Ratio 4

Authors: Paul G. Fournier
Categories: Airplanes
Type: BOOK - Published: 1953 - Publisher:

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The results presented in the present paper are part of a program conducted to investigate the effect of wing plan form on the aerodynamic characteristics in pit
Wind-tunnel Investigation at High Subsonic Speeds to Determine the Rolling Derivatives of Two Wing-fuselage Combinations Having Triangular Winds, Including a Semiempirical Method of Estimating the Rolling Derivatives
Language: en
Pages: 36

Wind-tunnel Investigation at High Subsonic Speeds to Determine the Rolling Derivatives of Two Wing-fuselage Combinations Having Triangular Winds, Including a Semiempirical Method of Estimating the Rolling Derivatives

Authors: James W. Wiggins
Categories: Airplanes
Type: BOOK - Published: 1954 - Publisher:

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The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds
Language: en
Pages: 86

The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds

Authors: Edward Charles Polhamus
Categories: Aerodynamics, Transonic
Type: BOOK - Published: 1960 - Publisher:

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Wind-tunnel Investigation of the Aerodynamic Characteristics in Pitch of Wing-fuselage Combinations at High Subsonic Speeds
Language: en
Pages: 36

Wind-tunnel Investigation of the Aerodynamic Characteristics in Pitch of Wing-fuselage Combinations at High Subsonic Speeds

Authors: Thomas J. King
Categories: Airplanes
Type: BOOK - Published: 1956 - Publisher:

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The results presented in the present paper represent a continuation of a research program conducted in the Langley high-speed 7- by 10-foot tunnel to investigat
The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds
Language: en
Pages: 90

The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds

Authors: Edward C. Polhamus
Categories: Aerodynamics
Type: BOOK - Published: 1955 - Publisher:

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A summary and analysis has been made of results obtained in a systematic research program concerned with the effects of wing sweep, aspect ratio, taper ratio, a