The Yawing Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow

The Yawing Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow PDF Author: Arthur Leslie Jones
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 72

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Book Description
The variation of the yawing moment with sideslip and the variation of the stability derivative with aspect ratio and Mach number were investigated.

The Yawing Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow

The Yawing Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow PDF Author: Arthur Leslie Jones
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 72

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Book Description
The variation of the yawing moment with sideslip and the variation of the stability derivative with aspect ratio and Mach number were investigated.

Rolling and Yawing Moments for Swept-back Wings in Sideslip at Supersonic Sppeds

Rolling and Yawing Moments for Swept-back Wings in Sideslip at Supersonic Sppeds PDF Author: Seymour Lampert
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 64

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Book Description
A method is presented for determining the rolling and yawing moments of swept-back wings in steady sideslip at supersonic speeds. The case treated in particular is that of a swept tapered wing with all edges subsonic.

Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 654

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Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces

Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces PDF Author: Arthur Earl Bryson
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 340

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Technical Information Pilot

Technical Information Pilot PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 694

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 446

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Technical Note

Technical Note PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 460

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Use of a Characteristic Surfaces for Unisymmetrical Supersonic Flow Problems

Use of a Characteristic Surfaces for Unisymmetrical Supersonic Flow Problems PDF Author: W. E. Moeckel
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 674

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Book Description
Application of the method of characteristics to the linearized three-dimensional equation results in a relatively simple system of difference equations that can be used to compute the supersonic flow past boundaries for which no other linearized solutions are available.

Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 498

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664

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