The Effect of Nacelle Combinations and Size on the Zero-lift Drag of a 45 Degrees Sweptback Wing and Body Configuration as Determined by Free-flight Tests at Mach Numbers Between 0.8 and 1.3

The Effect of Nacelle Combinations and Size on the Zero-lift Drag of a 45 Degrees Sweptback Wing and Body Configuration as Determined by Free-flight Tests at Mach Numbers Between 0.8 and 1.3 PDF Author: Sherwood Hoffman
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Category :
Languages : en
Pages :

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The Effect of Nacelle Location on the Zero-lift Drags of 45 Degrees Sweptback Wing-body Configurations Having Boattail and Cylindrical Afterbodies as Determined by Flight Tests at Transonic Speeds

The Effect of Nacelle Location on the Zero-lift Drags of 45 Degrees Sweptback Wing-body Configurations Having Boattail and Cylindrical Afterbodies as Determined by Flight Tests at Transonic Speeds PDF Author: Sherwood Hoffman
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Category :
Languages : en
Pages : 29

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Transonic Flight Tests to Compare the Zero-lift Drag on Underslung and Symmetrical Nacelles Varied Chordwise at 40 Percent Semispan of a 45© Sweptback, Tapered Wing

Transonic Flight Tests to Compare the Zero-lift Drag on Underslung and Symmetrical Nacelles Varied Chordwise at 40 Percent Semispan of a 45© Sweptback, Tapered Wing PDF Author: William B. Pepper
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Category : Airplanes
Languages : en
Pages : 40

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Comparison of Zero-lift Drag Determined by Flight Tests at Transonic Speeds of Pylon, Underslung, and Symmetrically Mounted Nacelles at 40 Percent Semispan of a 45 Degrees Sweptback Wing and Body Combination

Comparison of Zero-lift Drag Determined by Flight Tests at Transonic Speeds of Pylon, Underslung, and Symmetrically Mounted Nacelles at 40 Percent Semispan of a 45 Degrees Sweptback Wing and Body Combination PDF Author: Sherwood Hoffman
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Category :
Languages : en
Pages : 18

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Subsonic Investigation of Effects of Body Indentation on Zero-lift Drag Characteristics of a 45© Sweptback Wing-body Combination with Natural and Fixed Boundary-layer Transition Through a Range of Reynolds Number from 1 X 106 to 8 X 106

Subsonic Investigation of Effects of Body Indentation on Zero-lift Drag Characteristics of a 45© Sweptback Wing-body Combination with Natural and Fixed Boundary-layer Transition Through a Range of Reynolds Number from 1 X 106 to 8 X 106 PDF Author: Gene J. Bingham
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Category : Airplanes
Languages : en
Pages : 14

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Comparison of Zero-lift Drags Determined by Flight Tests at Transonic Speeds of Symmetrically Mounted Nacelles in Various Chordwise Positions at the Wing Tip of a 45 Degrees Sweptback Wing and Body Combination

Comparison of Zero-lift Drags Determined by Flight Tests at Transonic Speeds of Symmetrically Mounted Nacelles in Various Chordwise Positions at the Wing Tip of a 45 Degrees Sweptback Wing and Body Combination PDF Author: William B. Pepper
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Category :
Languages : en
Pages : 16

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Comparison of Zero-lift Drag Determined by Flight Tests at Transonic Speeds of Pylon, Underslung, and Symmetrically Mounted Nacelles at 40 Percenmt Semispan of a 45 Degree Sweptback Wing and Body Combination

Comparison of Zero-lift Drag Determined by Flight Tests at Transonic Speeds of Pylon, Underslung, and Symmetrically Mounted Nacelles at 40 Percenmt Semispan of a 45 Degree Sweptback Wing and Body Combination PDF Author: Sherwood Hoffman
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Category :
Languages : en
Pages : 18

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An Experimental Transonic Investigation of a 45© Sweptback Wing-body Combination with Several Types of Body Indentation with Theoretical Comparisons Included

An Experimental Transonic Investigation of a 45© Sweptback Wing-body Combination with Several Types of Body Indentation with Theoretical Comparisons Included PDF Author: Melvin M. Carmel
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Category : Aerodynamics, Transonic
Languages : en
Pages : 60

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Comparison of Zero-lift Drags Determined by Flight Tests at Transonic Speeds of Symmetrically Mounted Nacelles in Various Spanwise Positions on a 45 Degree Sweptback Wing and Body Combination

Comparison of Zero-lift Drags Determined by Flight Tests at Transonic Speeds of Symmetrically Mounted Nacelles in Various Spanwise Positions on a 45 Degree Sweptback Wing and Body Combination PDF Author: William B. Pepper
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ISBN:
Category :
Languages : en
Pages : 29

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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
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ISBN:
Category :
Languages : en
Pages : 20

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