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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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

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

Flight Tests to Determine the Effect of Taper on the Zero-lift Drag of Wings at Low Supersonic Speeds PDF Author: Sidney R. Alexander
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 8

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Book Description
Tests were conducted on wings having taper ratios from 0 to 1 mounted on rocket propelled test bodies to determine the effect of taper on the zero lift drag of wings at low supersonic speeds. Detailed data on models and test conditions are provided. comparison is made between results of theoretical drag calculations of tapered wings and applicable experimental values derived. Maximum thickness, leading edge, and trailing edge sweep are used in determining drag coefficient. At a constant leading edge sweep of 45 degree, no orderly variation of drag coefficient with taper ratio occurs.

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