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

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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

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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

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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

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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

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

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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

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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

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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

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Transonic Flight Tests to Determine Zero-lift Drag and Pressure Recovery of Nacelles Located at the Wing Root on a 45 Degree Sweptback Wing and Body Configuration

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