Longitudinal Stability Characteristics at Transonic Speeds of a Canard Configuration Having a 45 Degree Sweptback Wing of Aspect Ratio 6.0 and NACA 65A009 Airfoil Section

Longitudinal Stability Characteristics at Transonic Speeds of a Canard Configuration Having a 45 Degree Sweptback Wing of Aspect Ratio 6.0 and NACA 65A009 Airfoil Section PDF Author: A. James Vitale
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ISBN:
Category : Airplanes
Languages : en
Pages : 24

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Book Description
A flight investigation has been conducted to determine the longitudinal stability, lift, and drag characteristics at transonic speeds of a rocket-powered model of a canard configuration having a 45 degree swept-back wing of aspect ratio 6.0, taper ratio of 0.6, and NACA 65A009 airfoil section. The canard surface had an aspect ratio of 4.0 and 45 degrees of sweepback. The variations with Mach number of lift, drag, and longitudinal stability for the canard configuration are compared with a tailless and a conventional or tail-last model having the same wing.

Longitudinal Stability Characteristics at Transonic Speeds of a Canard Configuration Having a 45 Degree Sweptback Wing of Aspect Ratio 6.0 and NACA 65A009 Airfoil Section

Longitudinal Stability Characteristics at Transonic Speeds of a Canard Configuration Having a 45 Degree Sweptback Wing of Aspect Ratio 6.0 and NACA 65A009 Airfoil Section PDF Author: A. James Vitale
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 24

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Book Description
A flight investigation has been conducted to determine the longitudinal stability, lift, and drag characteristics at transonic speeds of a rocket-powered model of a canard configuration having a 45 degree swept-back wing of aspect ratio 6.0, taper ratio of 0.6, and NACA 65A009 airfoil section. The canard surface had an aspect ratio of 4.0 and 45 degrees of sweepback. The variations with Mach number of lift, drag, and longitudinal stability for the canard configuration are compared with a tailless and a conventional or tail-last model having the same wing.

Longitudinal Stability Characteristics at Transonic Speeds of a Canard Configuration Having a 45° Sweptback Wing of Aspect Ratio 6.0 and NACA 65A009 Airfoil Section

Longitudinal Stability Characteristics at Transonic Speeds of a Canard Configuration Having a 45° Sweptback Wing of Aspect Ratio 6.0 and NACA 65A009 Airfoil Section PDF Author: A. James Vitale
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 24

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Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Having a 45 Degree Swept Wing of Aspect Ratio 6.0

Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Having a 45 Degree Swept Wing of Aspect Ratio 6.0 PDF Author: John C. McFall
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 44

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Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 374

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author: United States. Superintendent of Documents
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ISBN:
Category : Government publications
Languages : en
Pages : 1714

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Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.

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
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ISBN:
Category : Airplanes
Languages : en
Pages : 38

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Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice PDF Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 508

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Research Abstracts

Research Abstracts PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 442

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Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Configuration Having a 45 Degree Swept Wing of Aspect Ratio 6.0

Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Configuration Having a 45 Degree Swept Wing of Aspect Ratio 6.0 PDF Author: John C. Jr McFall
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ISBN:
Category :
Languages : en
Pages : 34

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

Low-speed Static Longitudinal Stability Characteristics of a Canard Model Having a 60 Degree Triangular Wing and Horizontal Tail PDF Author: William R. Bates
Publisher:
ISBN:
Category :
Languages : en
Pages : 16

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Book Description