Download or read book The Pressure at the Base of Bodies at Supersonic Speeds written by H. H. Kurzweg and published by . This book was released on 1948 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: The designer of supersonic missiles needs accurate values of the aerodynamic forces and their distribution over the entire surface of the missile. Bodies with flat bases or blunt tails have a base drag which can be quite considerable at high speeds, thus playing an important part in the energy balance. Present knowledge of base pressures, particularly at high Mach numbers, is scanty. This report deals with this problem. The available data are discussed, the main test methods are subjected to critical study, and suggestions are made for further wind-tunnel measurements.

Download or read book Investigation of the Effect of Low Thrust Levels on the Base Pressure of a Cylindrical Body at Supersonic Speeds written by T. A. Martin and published by . This book was released on 1970 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results of supersonic wind tunnel tests are presented which show the effects of varying nozzle geometry, location, and supply pressure on the base pressure of a cylindrical body at zero angle of attack. The purpose of the tests was to investigate the parametric influences in the regions where base pressure is near a minimum, which occurs in the lower range of thrust levels. A bibliography of related experimental results is also included.

Download or read book Investigations at Supersonic Speeds of the Base Pressure on Bodies of Revolution with and Without Sweptback Stabilizing Fins written by Eugene S. Love and published by . This book was released on 1952 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory and published by . This book was released on 1950 with total page 372 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Base Pressure at Supersonic Speeds on Two dimensional Airfoils and Bodies of Revolution with and Without Fins Having Turbulent Boundary Layers written by Eugene S. Love and published by . This book was released on 1953 with total page 65 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Note on the Estimation of the Base Pressure on Bodies of Revolution at Supersonic Speeds written by L. E. Fraenkel and published by . This book was released on 1952 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Base Pressure at Supersonic Speeds on Two dimensional Airfoils and on Bodies of Revolution with and Without Fins Having Turbulent Boundary Layers written by Eugene S. Love and published by . This book was released on 1957 with total page 65 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analysis has been made of available experimental data to show the effects of most of the variables that are more predominant in determining base pressure at supersonic speeds. The analysis covers base pressures for two-dimensional airfoils and for bodies of revolution with and without stabilizing fins and is restricted to turbulent boundary layers. The present status of available experimental information is summarized as are the existing methods for predicting base pressure.

Download or read book Handbook of Supersonic Aerodynamics written by D. Adamson and published by . This book was released on 1961 with total page 366 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Inclined Bodies of Various Cross Sections at Supersonic Speeds written by Leland H. Jorgensen and published by . This book was released on 1958 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Jet Effects at Supersonic Speeds on Base and Afterbody Pressures of a Missile Model Having Single and Multiple Jets written by Nickolai Charczenko and published by . This book was released on 1963 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Technical Note National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1956 with total page 1026 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory and published by . This book was released on 1966 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind tunnel Investigation of a Number of Total pressure Tubes at High Angles of Attack written by A. Gerald Rainey and published by . This book was released on 1957 with total page 316 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Investigation at Supersonic Speeds of the Variation with Reynolds Number and Mach Number of the Total Base and Skin friction Drag of Seven Boattail Bodies of Revolution Designed for Minimum Wave Drag written by August F. Bromm and published by . This book was released on 1953 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerodynamics of Bodies of Revolution written by Nikolaĭ Fedorovich Krasnov and published by Elsevier Publishing Company. This book was released on 1970 with total page 930 pages. Available in PDF, EPUB and Kindle. Book excerpt: A comprehensive technical treatise is provided on the aerodynamics of bodies of revolution from transonic to hypersonic speeds, covering all aspects of the subject, including transonic flow, linearized supersonic flow, Newtonian flow, rarefield gas and free-molecule flow, skin friction, heat transfer, and mass transfer. This English translation of a unique Russian textbook is provided with some corrections, references for all sources the editor could identify, redrawn figures, and an editor's introduction to each chapter summarizing and referencing pertinent material that has appeared since 1964, when the second edition was published. Krasnov's general approach assumes knowledge of the basic gas dynamic equations and applies them to solve aerodynamic problems. All important methods and techniques in modern aerodynamic theory are developed, with the aim of presenting practical methods for solving engineering problems. Results are usually given in the form of working equations, graphs, tables, or detailed sequential calculation methods. (Author).

Download or read book Pressure Distribution on Bodies of Revolution at Supersonic Speeds written by M.H. Gheith and published by . This book was released on 1978 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Summary of Information on Support Interference at Transonic and Supersonic Speeds written by Eugene S. Love and published by . This book was released on 1954 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: A compilation of available information on the problem of support interference at transonic and supersonic speeds is presented.