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Aerodynamic Characteristics For Cone Cylinder Frustum Cylinder Configurations At Mach Numbers From 07 To 196
Download Aerodynamic Characteristics For Cone Cylinder Frustum Cylinder Configurations At Mach Numbers From 07 To 196 full books in PDF, epub, and Kindle. Read online Aerodynamic Characteristics For Cone Cylinder Frustum Cylinder Configurations At Mach Numbers From 07 To 196 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Aerodynamic Characteristics for Cone Cylinder Frustum Cylinder Configurations at Mach Numbers from 0.7 T0 1.96 by : J.F. Thompson
Download or read book Aerodynamic Characteristics for Cone Cylinder Frustum Cylinder Configurations at Mach Numbers from 0.7 T0 1.96 written by J.F. Thompson and published by . This book was released on 1967 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics for Cone-cylinder-frustum-cylinder Configurations at Mach Numbers from 0.7 to 1.96 by : J. F. Thompson
Download or read book Aerodynamic Characteristics for Cone-cylinder-frustum-cylinder Configurations at Mach Numbers from 0.7 to 1.96 written by J. F. Thompson and published by . This book was released on 1967 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics for Cone-cylinder-frustum-cylinder Configurations at Mach Numbers from 0.7 to 1.96 by : J. F. Thompson
Download or read book Aerodynamic Characteristics for Cone-cylinder-frustum-cylinder Configurations at Mach Numbers from 0.7 to 1.96 written by J. F. Thompson and published by . This book was released on 1967 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300 by : Jim A. Penland
Download or read book Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300 written by Jim A. Penland and published by . This book was released on 1961 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Modified Cone by : George C. Ashby
Download or read book Aerodynamic Characteristics of a Modified Cone written by George C. Ashby and published by . This book was released on 1968 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 130 Degrees by : JIM A. PENLAND
Download or read book Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 130 Degrees written by JIM A. PENLAND and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: Force tests of a series of right circular cones having semivertex angles ranging from 5 to 45 degrees and a series of right circular cone-cylinder configurations having semivertex angles ranging from 5 to 20 degrees and an afterbody fineness ratio of 6 have been made in the Langley 11inch hypersonic tunnel at a Mach number of 6.83, a Reynolds number of 0.24 x 10 to the 6th power per inch, and angles of attack up to 130 degrees. An analysis of the results made use of the Newtonian and modified Newtonian theories and the exact theory. A comparison of the experimental data of both cone and cone-cylinder configurations with theoretical calculations shows that the Newtonian concept gives excellent predictions of trends of the force characteristics and the locations with respect to angle of attack of the points of maximum lift, maximum drag, and maximum lift-drag ratio. Both the Newtonian and exact theories give excellent predictions of the sign and value of the initial lift-curve slope. (Author).
Book Synopsis Longitudinal Aerodynamic Characteristics of Two Blunted Cone Reentry Configurations at Mach Numbers from 17.6 to 22.2 Including Some Reynolds Number Effects by : Dal V. Maddalon
Download or read book Longitudinal Aerodynamic Characteristics of Two Blunted Cone Reentry Configurations at Mach Numbers from 17.6 to 22.2 Including Some Reynolds Number Effects written by Dal V. Maddalon and published by . This book was released on 1966 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation of the Aerodynamic Characteristics of a Series of Cone-cylinder Configurations at a Mach Number of 6.86 by : Ralph D. Cooper
Download or read book An Investigation of the Aerodynamic Characteristics of a Series of Cone-cylinder Configurations at a Mach Number of 6.86 written by Ralph D. Cooper and published by . This book was released on 1951 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Afterbody Shape on the Aerodynamic Characteristics of a Fineness-ratio-10 Cone- Cylinder Configuration at Mach Numbers from 1.57 to 4.65 Including Design Parameter Curves for Circular Afterbody Flares by : A. B. Carraway
Download or read book Effects of Afterbody Shape on the Aerodynamic Characteristics of a Fineness-ratio-10 Cone- Cylinder Configuration at Mach Numbers from 1.57 to 4.65 Including Design Parameter Curves for Circular Afterbody Flares written by A. B. Carraway and published by . This book was released on 1960 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Static Stability Characteristics of Several Cone-cylinder-flare-cylinder Configurations at Mach Numbers 0.4 to 4.5 by : D. J. Spring
Download or read book The Static Stability Characteristics of Several Cone-cylinder-flare-cylinder Configurations at Mach Numbers 0.4 to 4.5 written by D. J. Spring and published by . This book was released on 1963 with total page 270 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic characteristics of various cone cylinder-flare-skirt configurations were inves tigated between Mach Numbers 0.4 to 4.5. The Reynolds number range for the tests was from 0.5 to 6.0 million per foot. Data are presented in basic form, along with cross plots, to show the effect of changing various body component shapes. (Author).
Book Synopsis Supersonic Aerodynamic Characteristics and Shock Standoff Distances for Large-angle Cones with and Without Cylindrical Afterbodies by : James Franklin Campbell
Download or read book Supersonic Aerodynamic Characteristics and Shock Standoff Distances for Large-angle Cones with and Without Cylindrical Afterbodies written by James Franklin Campbell and published by . This book was released on 1969 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: Supersonic aerodynamic characteristics and shock standoff distances for large angle cones with and without cylindrical afterbodies.
Book Synopsis Aerodynamic Characteristics of a Modified Cone-conical-frustum Entry Configuration at Mach 6.0 by : George C. Ashby
Download or read book Aerodynamic Characteristics of a Modified Cone-conical-frustum Entry Configuration at Mach 6.0 written by George C. Ashby and published by . This book was released on 1968 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 130° by : Jim A. Penland
Download or read book Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 130° written by Jim A. Penland and published by . This book was released on 1961 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Towed Spheres, Conical Rings, and Cones Used as Decelerators at Mach Numbers from 1.57 to 4.65 by : Nickolai Charczenko
Download or read book Aerodynamic Characteristics of Towed Spheres, Conical Rings, and Cones Used as Decelerators at Mach Numbers from 1.57 to 4.65 written by Nickolai Charczenko and published by . This book was released on 1963 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made to determine the drag and stability characteristics of the various decelerators when towed in the wake of several space-vehicle configurations at Mach numbers from 1.57 to 4.65. The following parameters were varied: Reynolds number, trailling distance, ratio of deceleration base diameter to space-vehicle base diameter, cone angle, and size of disk added to the base of a cone.
Book Synopsis Subsonic High-angle-of-attack Aerodynamic Characteristics of a Cone and Cylinder with Triangular Cross Sections and a Cone with a Square Cross Section by :
Download or read book Subsonic High-angle-of-attack Aerodynamic Characteristics of a Cone and Cylinder with Triangular Cross Sections and a Cone with a Square Cross Section written by and published by . This book was released on 1983 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics of Blunted Cones at Mach Numbers of 3.5, 4.2, and 6.0 by : J. Wayne Keyes
Download or read book Longitudinal Aerodynamic Characteristics of Blunted Cones at Mach Numbers of 3.5, 4.2, and 6.0 written by J. Wayne Keyes and published by . This book was released on 1964 with total page 72 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 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
