Wind-tunnel Investigation at Low Speed of Lateral Control Characteristics of an Untapered 45 [degress] Sweptback Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Ailerons PDF Download

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Wind-tunnel Investigation at Low Speed of Lateral Control Characteristics of an Untapered 45 [degress] Sweptback Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Ailerons

Wind-tunnel Investigation at Low Speed of Lateral Control Characteristics of an Untapered 45 [degress] Sweptback Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Ailerons PDF Author: Harold S. Johnson
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

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Wind-tunnel Investigation at Low Speed of Lateral Control Characteristics of an Untapered 45 [degress] Sweptback Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Ailerons

Wind-tunnel Investigation at Low Speed of Lateral Control Characteristics of an Untapered 45 [degress] Sweptback Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Ailerons PDF Author: Harold S. Johnson
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

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Book Description

Wind-tunnel Investigation at Low Speed of Lateral Control Characteristics of an Untapered 45 Degrees Sweptback Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Ailerons

Wind-tunnel Investigation at Low Speed of Lateral Control Characteristics of an Untapered 45 Degrees Sweptback Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Ailerons PDF Author: Harold S. Johnson
Publisher:
ISBN:
Category :
Languages : en
Pages :

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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 : 258

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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 : 750

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Wind-tunnel Investigation at Low Speed of a 45° Sweptback Untapered Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Flaps

Wind-tunnel Investigation at Low Speed of a 45° Sweptback Untapered Semispan Wing of Aspect Ratio 1.59 Equipped with Various 25-percent-chord Plain Flaps PDF Author: Harold S. Johnson
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

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Wind-tunnel Investigation at Low Speed of the Effect of Varying the Ratio of Body Diameter to Wing Span from 0.1 to 0.8 on the Aerodynamic Characteristics in Pitch of the 45© Sweptback-wing--body Combination

Wind-tunnel Investigation at Low Speed of the Effect of Varying the Ratio of Body Diameter to Wing Span from 0.1 to 0.8 on the Aerodynamic Characteristics in Pitch of the 45© Sweptback-wing--body Combination PDF Author: Harold S. Johnson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36

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Measurements of Section Characteristics of a 45 Degree Swept Wing Spanning a Rectangular Low-speed Wind Tunnel as Affected by the Tunnel Walls

Measurements of Section Characteristics of a 45 Degree Swept Wing Spanning a Rectangular Low-speed Wind Tunnel as Affected by the Tunnel Walls PDF Author: Robert E. Dannenberg
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 678

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Book Description
Tunnel-wall corrections for the induced upwash velocity for a swept wing completely spanning a rectangular wind tunnel are included in the appendix.

Some Low-speed Wind-tunnel Experiments Pertaining to the Longitudinal Stability Characteristics of a 35© Swept-wing Model and an Unswept-wing Model

Some Low-speed Wind-tunnel Experiments Pertaining to the Longitudinal Stability Characteristics of a 35© Swept-wing Model and an Unswept-wing Model PDF Author: Byron M. Jaquet
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 48

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Transonic Wind-tunnel Investigation of the Effects of Sweepback and Thickness Ratio on the Wing Loads of a Wing-body Combination of Aspect Ratio 4 and Taper Ratio 0.6

Transonic Wind-tunnel Investigation of the Effects of Sweepback and Thickness Ratio on the Wing Loads of a Wing-body Combination of Aspect Ratio 4 and Taper Ratio 0.6 PDF Author: Robert J. Platt
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 50

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Book Description
A transonic investigation of the effects of sweepback and thickness ratio on the wing loads of a wing in the presence of a body has been made in the Langley 8-foot transonic pressure tunnel. The tests covered wings with a thickness ratio of 6 percent for sweepback angles of 0, 25, and 45 degrees and a thickness ratio of 4 percent for an unswept wing.

A Wind-tunnel Investigation at Low Speed of Various Lateral Controls on a 45 Degree Swept-back Wing

A Wind-tunnel Investigation at Low Speed of Various Lateral Controls on a 45 Degree Swept-back Wing PDF Author: Edward J. Hopkins
Publisher:
ISBN:
Category :
Languages : en
Pages : 22

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Book Description