Transonic Flight Tests to Determine the Effect of Thickness Ratio and Plan-form Modification on the Zero-lift Drag of a 45© Sweptback Wing PDF Download

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Transonic Flight Tests to Determine the Effect of Thickness Ratio and Plan-form Modification on the Zero-lift Drag of a 45© Sweptback Wing

Transonic Flight Tests to Determine the Effect of Thickness Ratio and Plan-form Modification on the Zero-lift Drag of a 45© Sweptback Wing PDF Author: William B. Pepper
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 28

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Book Description

Transonic Flight Tests to Determine the Effect of Thickness Ratio and Plan-form Modification on the Zero-lift Drag of a 45© Sweptback Wing

Transonic Flight Tests to Determine the Effect of Thickness Ratio and Plan-form Modification on the Zero-lift Drag of a 45© Sweptback Wing PDF Author: William B. Pepper
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 28

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Book Description

Effect of Some Section Modifications and Protuberances on the Zero-lift Drag of Delta Wings at Transonic and Supersonic Speeds

Effect of Some Section Modifications and Protuberances on the Zero-lift Drag of Delta Wings at Transonic and Supersonic Speeds PDF Author: Carl A. Sandahl
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 48

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Book Description

Transonic Flight Tests to Compare the Zero-lift Drags of 45 Degrees Sweptback Wings of Aspect Ratio 3.55 and 6.0 with and Without Nacelles at the Wing Tips

Transonic Flight Tests to Compare the Zero-lift Drags of 45 Degrees Sweptback Wings of Aspect Ratio 3.55 and 6.0 with and Without Nacelles at the Wing Tips PDF Author: Sherwood Hoffman
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Flight Tests at Supersonic Speeds to Determine the Effect of Taper on the Zero-lift Drag of Sweptback Low-aspect-ratio Wings

Flight Tests at Supersonic Speeds to Determine the Effect of Taper on the Zero-lift Drag of Sweptback Low-aspect-ratio Wings PDF Author: Murray Pittel
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 20

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Book Description
Rocket-powered models have been flown to provide an experimental comparison with linearized theoretical calculations for zero-lift drag of sweptback tapered wings having thin, symmetrical, double-wedge airfoil sections. The range of the experimental data is from a Mach number M of 1.0 to 1.8, and theoretical comparisons are made for the test range above M = 1.2.

Transonic Flight Tests to Compare the Zero-lift Drags of 45 Degree Sweptback Wings of Aspect Ratio 3.55 and 6.0 with and Without Nacelles at the Wing Tips

Transonic Flight Tests to Compare the Zero-lift Drags of 45 Degree Sweptback Wings of Aspect Ratio 3.55 and 6.0 with and Without Nacelles at the Wing Tips PDF Author: Sherwood Hoffman
Publisher:
ISBN:
Category :
Languages : en
Pages : 17

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Book Description

The Effect on Zero-lift Drag of an Indented Fuselage Or a Thickened Wing-root Modification to a 45 Degrees Sweptback Wing-body Configuration as Determined by Flight Tests at Transonic Speeds

The Effect on Zero-lift Drag of an Indented Fuselage Or a Thickened Wing-root Modification to a 45 Degrees Sweptback Wing-body Configuration as Determined by Flight Tests at Transonic Speeds PDF Author: William B. Pepper
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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Book Description

Flight Tests to Determine the Effect of Airfoil Section Profile and Thickness Ratio on the Zero-Lift Drag of Low-Aspect Ratio Wings at Supersonic Speeds

Flight Tests to Determine the Effect of Airfoil Section Profile and Thickness Ratio on the Zero-Lift Drag of Low-Aspect Ratio Wings at Supersonic Speeds PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 19

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Book Description

Transonic Flight Tests to Determine Zero-lift Drag and Pressure Recovery of Nacelles Located at the Wing Tips on a 45 Degrees Sweptback Wing and Body Combination

Transonic Flight Tests to Determine Zero-lift Drag and Pressure Recovery of Nacelles Located at the Wing Tips on a 45 Degrees Sweptback Wing and Body Combination PDF Author: Sherwood Hoffman
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Book Description

The Effect on Zero-lift Drag of an Indented Fuselage Or a Thickened Wing-root Modification to a 45° Sweptback Wing-body Configuration as Determined by Flight Tests at Transonic Speeds

The Effect on Zero-lift Drag of an Indented Fuselage Or a Thickened Wing-root Modification to a 45° Sweptback Wing-body Configuration as Determined by Flight Tests at Transonic Speeds PDF Author: William B. Pepper
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 20

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Book Description

Large-scale Flight Measurements of Zero-lift Drag and Low-lift Drag of 10 Wing-body Configurations at Mach Numbers from 0.8 to 1.6

Large-scale Flight Measurements of Zero-lift Drag and Low-lift Drag of 10 Wing-body Configurations at Mach Numbers from 0.8 to 1.6 PDF Author: John D. Morrow
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 58

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Book Description