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Book Static Aerodynamic Characteristics of a Single stage to orbit Vehicle with Low Planform Loading at Mach Numbers from 0 3 to 4 63

Download or read book Static Aerodynamic Characteristics of a Single stage to orbit Vehicle with Low Planform Loading at Mach Numbers from 0 3 to 4 63 written by Delma C. Freeman and published by . This book was released on 1977 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static aerodynamic characteristics of a single stage to orbit vehicle with low planform loading at Mach numbers from 0 3 to 4 63

Download or read book Static aerodynamic characteristics of a single stage to orbit vehicle with low planform loading at Mach numbers from 0 3 to 4 63 written by Delma C. Freeman and published by . This book was released on 1977 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerodynamic Data of Space Vehicles

Download or read book Aerodynamic Data of Space Vehicles written by Claus Weiland and published by Springer Science & Business Media. This book was released on 2014-02-22 with total page 360 pages. Available in PDF, EPUB and Kindle. Book excerpt: The capacity and quality of the atmospheric flight performance of space flight vehicles is characterized by their aerodynamic data bases. A complete aerodynamic data base would encompass the coefficients of the static longitudinal and lateral motions and the related dynamic coefficients. In this book the aerodynamics of 27 vehicles are considered. Only a few of them did really fly. Therefore the aerodynamic data bases are often not complete, in particular when the projects or programs were more or less abruptly stopped, often due to political decisions. Configurational design studies or the development of demonstrators usually happen with reduced or incomplete aerodynamic data sets. Therefore some data sets base just on the application of one of the following tools: semi-empirical design methods, wind tunnel tests, numerical simulations. In so far a high percentage of the data presented is incomplete and would have to be verified. Flight mechanics needs the aerodynamic coefficients as function of a lot of variables. The allocation of the aerodynamic coefficients for a particular flight operation at a specific trajectory point is conducted by an aerodynamic model. The establishment of such models is described in this book. This book is written for graduate and doctoral students to give them insight into the aerodynamics of the various flight configurations. Further for design and development engineers in industry and at research institutes (including universities) searching for an appropriate vehicle shape, as well as for non-specialists, who may be interested in this subject. The book will be helpful, too, in the case that system studies require in their concept phases the selection of suitable vehicle shapes.

Book Aerodynamic Characteristics of Two Single Stage To Orbit Vehicles at Mach 20 3

Download or read book Aerodynamic Characteristics of Two Single Stage To Orbit Vehicles at Mach 20 3 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-22 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: The hypersonic stability, control, and performance characteristics of two configurations have been determined. Each configuration had a 50 deg swept delta wing, a vertical tail, and a body flap. One model represented a control configured vehicle with a reduced level of longitudinal static stability; the other model was designed for a conventional level of stability. Data were obtained over an angle of attack range of 0 deg to 50 deg and included effects of component buildup. In addition, the effects of the vertical tail on the lateral directional characteristics were obtained. Bernot, P. T. Langley Research Center NASA-TM-X-3550, L-11627 RTOP 506-26-10-08...

Book Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1 57 to 4 65

Download or read book Aerodynamic Characteristics of Several Proposed Versions of the Saturn V Launch Vehicle at Mach Numbers 1 57 to 4 65 written by Dennis E. Fuller and published by . This book was released on 1964 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Stability Investigations of Proposed Project Fire Space vehicle and Reentry package Configurations at Mach Numbers from 1 47 to 4 63

Download or read book Static Stability Investigations of Proposed Project Fire Space vehicle and Reentry package Configurations at Mach Numbers from 1 47 to 4 63 written by Dennis E. Fuller and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Aerodynamic Characteristics of a Series of Generalized Slender Bodies with and Without Fins at Mach Numbers Form 0 6 to 3 0 and Angles of Attack from 0 to 180 Deg

Download or read book Static Aerodynamic Characteristics of a Series of Generalized Slender Bodies with and Without Fins at Mach Numbers Form 0 6 to 3 0 and Angles of Attack from 0 to 180 Deg written by William B. Baker (Jr.) and published by . This book was released on 1976 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Aerodynamic Characteristics of a Model of a Saturn 1 Block 2 Launch Vehicle with Proposed Spacecraft at Mach Numbers from 1 57 to 2 87

Download or read book Static Aerodynamic Characteristics of a Model of a Saturn 1 Block 2 Launch Vehicle with Proposed Spacecraft at Mach Numbers from 1 57 to 2 87 written by and published by . This book was released on 1964 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Longitudinal Aerodynamic Characteristics of Several Configurations Used in the Development of the Little Joe II Apollo Test Vehicle at Mach Numbers from 0 056 to 4 65

Download or read book Static Longitudinal Aerodynamic Characteristics of Several Configurations Used in the Development of the Little Joe II Apollo Test Vehicle at Mach Numbers from 0 056 to 4 65 written by Robert H. Moore and published by . This book was released on 1968 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Effects of Reynolds Number and Body Corner Radius on Aerodynamic Characteristics of a Space Shuttle type Vehicle at Subsonic Mach Numbers

Download or read book Effects of Reynolds Number and Body Corner Radius on Aerodynamic Characteristics of a Space Shuttle type Vehicle at Subsonic Mach Numbers written by Leland Howard Jorgenson and published by . This book was released on 1972 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Static aerodynamic forces and moments were measured to study the effects of Reynolds number and body corner radius on the aerodynamic characteristics of a straight wing space shuttle orbiter at subsonic speeds. A 0.02-scale model was tested at Mach numbers from 0.3 to 0.9 and Reynolds numbers from about 600,000 to 3 million, based on body width. The body alone and the body with its wing and horizontal tail attached were tested at angles of attack from 35 to 75 degrees. The effects of rounding the body corners at the junctures connecting the bottom and sides were investigated for corner radii from 0 to 8.5 percent of the body width. At low subsonic Mach numbers (free stream Mach number approximately equal 0.3) the aerodynamic characteristics are affected significantly by changes in Reynolds number and body corner radius. With increase in Mach number to free stream Mach number = 0.9 the effect of Reynolds number seems to vanish, but a significant effect of body corner radius remains.