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Longitudinal Aerodynamic Characteristics Of Several High Drag Bodies At Mach Numbers From 150 To 463
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Book Synopsis Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 by : James F. Campbell
Download or read book Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 written by James F. Campbell and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 by : James F. Campbell
Download or read book Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 written by James F. Campbell and published by . This book was released on 1967 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Performance of a Series of Power-law and Minimum-wave-drag Bodies at Mach 6 and Several Reynolds Numbers by : George C. Ashby
Download or read book Longitudinal Aerodynamic Performance of a Series of Power-law and Minimum-wave-drag Bodies at Mach 6 and Several Reynolds Numbers written by George C. Ashby and published by . This book was released on 1974 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing by : Edward J. Ray
Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing written by Edward J. Ray and published by . This book was released on 1967 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG by :
Download or read book STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT-BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6.8 AND ANGLES OF ATTACK UP TO 90 DEG written by and published by . This book was released on 1959 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation at a Mach Number of 2.01 of the Effects of Body Cross-section Shape on the Aerodynamic Characteristics of Bodies and Wing-body Combinations by : Harry W. Carlson
Download or read book An Experimental Investigation at a Mach Number of 2.01 of the Effects of Body Cross-section Shape on the Aerodynamic Characteristics of Bodies and Wing-body Combinations written by Harry W. Carlson and published by . This book was released on 1955 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: An experimental investigation has been performed to determine the effect of changes in body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations. A series of 13 bodies having a given length and given longitudinal distribution of cross-sectional area but various cross-section shapes were tested at a Mach number of 2.01. The bodies were tested alone and in combination with a 47° sweptback wing having a 6-percent-thick hexagonal section.
Book Synopsis The Longitudinal Aerodynamic Characteristics of a Sweptback Wing-body Combination with and Without End Plates at Mach Numbers from 0.40 to 0.93 by : W. P. Henderson
Download or read book The Longitudinal Aerodynamic Characteristics of a Sweptback Wing-body Combination with and Without End Plates at Mach Numbers from 0.40 to 0.93 written by W. P. Henderson and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers 2.30, 2.60, and 2.96 of a Supersonic Transport Model Having a Fixed, Warped Wing by :
Download or read book Aerodynamic Characteristics at Mach Numbers 2.30, 2.60, and 2.96 of a Supersonic Transport Model Having a Fixed, Warped Wing written by and published by . This book was released on 1965 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics of a High-subsonic-speed Transport Airplane Model with a Cambered 40 Deg Sweptback Wing of Aspect Ratio 8 at Mach Numbers to 0.96 by :
Download or read book Longitudinal Aerodynamic Characteristics of a High-subsonic-speed Transport Airplane Model with a Cambered 40 Deg Sweptback Wing of Aspect Ratio 8 at Mach Numbers to 0.96 written by and published by . This book was released on 1960 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics at a Mach Number of 1.97 of a Series of Related Winged Reentry Configurations for Angles of Attack from 0 Deg to 90 Deg by :
Download or read book Longitudinal Aerodynamic Characteristics at a Mach Number of 1.97 of a Series of Related Winged Reentry Configurations for Angles of Attack from 0 Deg to 90 Deg written by and published by . This book was released on 1961 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 3.00, 3.96, and 4.65 of a Low-fineness-ratio Elliptical Hypersonic Configuration Having Variable-sweep Wing Panels by :
Download or read book Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers of 3.00, 3.96, and 4.65 of a Low-fineness-ratio Elliptical Hypersonic Configuration Having Variable-sweep Wing Panels written by and published by . This book was released on 1963 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Some Modified Conical Bodies with Low Lift Drag Ratios at Mach Numbers of 2.30 and 4.63 by : Edwin E. Davenport
Download or read book Aerodynamic Characteristics of Some Modified Conical Bodies with Low Lift Drag Ratios at Mach Numbers of 2.30 and 4.63 written by Edwin E. Davenport and published by . This book was released on 1972 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Aerodynamic Characteristics of a Series of Related Bodies with Cross-sectional Ellipticity by : Bernard Spencer
Download or read book Transonic Aerodynamic Characteristics of a Series of Related Bodies with Cross-sectional Ellipticity written by Bernard Spencer and published by . This book was released on 1966 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 0.50 to 2.96 of a Supersonic Transport Model with a Variable-sweep High-panel-aspect-ratio Wing by :
Download or read book Aerodynamic Characteristics at Mach Numbers from 0.50 to 2.96 of a Supersonic Transport Model with a Variable-sweep High-panel-aspect-ratio Wing written by and published by . This book was released on 1964 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 4.63 of an Airplane with a Translating Horizontal Tail by :
Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 4.63 of an Airplane with a Translating Horizontal Tail written by and published by . This book was released on 1967 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Lee-surface Volume Addition on Longitudinal Aerodynamics of a High-lift-drag-ratio Wing-body Configuration at Mach 6.0 by : David R. Stone
Download or read book Effects of Lee-surface Volume Addition on Longitudinal Aerodynamics of a High-lift-drag-ratio Wing-body Configuration at Mach 6.0 written by David R. Stone and published by . This book was released on 1968 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack from -10 Degrees to 53 Degrees at Mach Numbers from 2.30 to 4.62 by : M. Leroy Spearman
Download or read book Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack from -10 Degrees to 53 Degrees at Mach Numbers from 2.30 to 4.62 written by M. Leroy Spearman and published by . This book was released on 1994 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
