Transonic Wind-tunnel Investigation of the Effects of Aspect Ratio, Spanwise Variations in Section Thickness Ratio, and a Body Indentation on the Aerodynamic Characteristics of a 45© Sweptback Wing-body Combination

Transonic Wind-tunnel Investigation of the Effects of Aspect Ratio, Spanwise Variations in Section Thickness Ratio, and a Body Indentation on the Aerodynamic Characteristics of a 45© Sweptback Wing-body Combination PDF Author: Melvin M. Carmel
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 50

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Transonic Wind-tunnel Investigation of the Effects of Aspect Ratio, Spanwise Variations in Section Thickness Ratio, and a Body Indentation on the Aerodynamic Characteristics of a 45 Degree Sweptback Wing-body Combination

Transonic Wind-tunnel Investigation of the Effects of Aspect Ratio, Spanwise Variations in Section Thickness Ratio, and a Body Indentation on the Aerodynamic Characteristics of a 45 Degree Sweptback Wing-body Combination PDF Author: Melvin M. Carmel
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ISBN:
Category :
Languages : en
Pages : 44

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A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of a 45 Degree Sweptback-wing-body Combination

A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of a 45 Degree Sweptback-wing-body Combination PDF Author: Harold L. Robinson
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Category :
Languages : en
Pages : 33

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A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of a 45 Degrees Sweptback-wing-body Combination

A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of a 45 Degrees Sweptback-wing-body Combination PDF Author: Harold L. Robinson
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Category :
Languages : en
Pages :

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Transonic Wind-tunnel Investigation of the Effects of Taper Ratio and Body Indentation on the Aerodynamic Loading Characteristics of a 45° Sweptback Wing in the Presence of a Body

Transonic Wind-tunnel Investigation of the Effects of Taper Ratio and Body Indentation on the Aerodynamic Loading Characteristics of a 45° Sweptback Wing in the Presence of a Body PDF Author: James Benjamin Delano
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ISBN:
Category : Aerodynamic load
Languages : en
Pages : 53

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A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of an Unswept-wing-body Combination

A Transonic Wind-tunnel Investigation of the Effects of Body Indentation, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of an Unswept-wing-body Combination PDF Author: Claude V. Williams
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Category :
Languages : en
Pages :

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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 a 45 Degree 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 a 45 Degree Sweptback-wing-body Combination PDF Author: Harold S. Johnson
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Category :
Languages : en
Pages : 32

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Transonic Wind-tunnel Investigation of the Effects of Body Indentation on the Aerodynamic Characteristics of a Semielliptical Sweptback Wing-root Inlet Configuration

Transonic Wind-tunnel Investigation of the Effects of Body Indentation on the Aerodynamic Characteristics of a Semielliptical Sweptback Wing-root Inlet Configuration PDF Author: Arvid L. Jr Keith
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Category :
Languages : en
Pages : 22

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A Transonic Wind-tunnel Investigation of the Aerodynamic Characteristics of Three 4-percent-thick Wings of Sweepback Angles 10.8 Degrees, 35 Degrees, and 47 Degrees, Aspect Ratio 3.5, and Taper Ratio 0.2 in Coombination with a Body

A Transonic Wind-tunnel Investigation of the Aerodynamic Characteristics of Three 4-percent-thick Wings of Sweepback Angles 10.8 Degrees, 35 Degrees, and 47 Degrees, Aspect Ratio 3.5, and Taper Ratio 0.2 in Coombination with a Body PDF Author: Ralph P. Bielat
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ISBN:
Category :
Languages : en
Pages : 33

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A Transonic Wind-tunnel Investigation of the Effects of Body Indention, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of an Unswept-wing-body Combination

A Transonic Wind-tunnel Investigation of the Effects of Body Indention, as Specified by the Transonic Drag-rise Rule, on the Aerodynamic Characteristics and Flow Phenomena of an Unswept-wing-body Combination PDF Author: Claude V. Williams
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

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