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Helium Injection Into The Boundary Layer At An Axisymmetric Stagnation Point
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Book Synopsis Helium Injection Into the Boundary Layer at an Axisymmetric Stagnation Point by : Herbert Fox
Download or read book Helium Injection Into the Boundary Layer at an Axisymmetric Stagnation Point written by Herbert Fox and published by . This book was released on 1961 with total page 210 pages. Available in PDF, EPUB and Kindle. Book excerpt: A theoretical analysis of the boundary layer at an axisymmetric stagnation point with large rates of helium injection is presented. The exact stagnation point boundary layer equations are integrated numerically with an approximate representation of the gas properties. The new treatment of the two-point boundary value problem that arises is shown to be useful for various boundary layer and mixing problems. The exact solutions indicate that for large rates of injection the boundary layer can be represented by a thick, inner layer of constant shear, temperature and composition and by a relatively thin outer region in which the flow variables adjust to their free-stream values. An inviscid flow model is shown to lead to accurate predictions of this shear layer and will thus provide sufficiently accurate profiles forfagnation point mass transfer. The heat transfer to the stagnation point is also considered. Tabulations of the solutawlconditions and injection rates are given in an appendix.
Book Synopsis Homogeneous Boundary Layer at an Axisymmetric Stagnation Point with Large Rates of Injection by : Paul A. Libby
Download or read book Homogeneous Boundary Layer at an Axisymmetric Stagnation Point with Large Rates of Injection written by Paul A. Libby and published by . This book was released on 1961 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Technical Abstract Bulletin by : Defense Documentation Center (U.S.)
Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1961-07 with total page 1766 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1971 with total page 776 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1967 with total page 346 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1962 with total page 182 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Helium written by Carla W. Cherry and published by . This book was released on 1968 with total page 536 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Information Circular written by and published by . This book was released on 1968 with total page 978 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Inviscid Hypersonic Flow Over a Blunt Body with High Rates of Mass and Heat Transfer by : Elmer Dale Martin
Download or read book Inviscid Hypersonic Flow Over a Blunt Body with High Rates of Mass and Heat Transfer written by Elmer Dale Martin and published by . This book was released on 1968 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Laminar-boundary-layer Displacement on a Hemisphere in Helium Flow by : Davis H. Crawford
Download or read book Effects of Laminar-boundary-layer Displacement on a Hemisphere in Helium Flow written by Davis H. Crawford and published by . This book was released on 1964 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Propulsion Re-Entry Physics by : Michał Lunc
Download or read book Propulsion Re-Entry Physics written by Michał Lunc and published by Elsevier. This book was released on 2014-05-09 with total page 613 pages. Available in PDF, EPUB and Kindle. Book excerpt: Propulsion Re-Entry Physics deals with the physics of propulsion re-entry and covers topics ranging from inductive magnetoplasmadynamic (MPD) propulsion systems to launch systems and orbiting maneuvering systems. Problems of re-entry aerodynamics are considered, along with interaction problems in hypersonic fluid dynamics. Comprised of 31 chapters, this volume begins with a detailed account of the quasi-steady adiabatic vaporization and subsequent exothermic decomposition of a pure monopropellant spherical droplet in the absence of free and forced convection. The discussion then turns to results of calculations on MPD machines working in the intermittent and in the continuous mode; inductive plasma accelerators with electromagnetic standing waves; and spherical rocket motors for space and upper stage propulsion. Subsequent chapters focus on pulsed plasma satellite control systems; drag and stability of various Mars entry configurations; hypersonic laminar boundary layers around slender bodies; and effects of an entry probe gas envelope on experiments concerning planetary atmospheres. This book will appeal to students, practitioners, and research workers interested in propulsion re-entry and the accompanying physics.
Book Synopsis Preliminary Analysis of the Capabilities of a Composite Slab for an Advanced Heat-sink Design by : Paul A. Libby
Download or read book Preliminary Analysis of the Capabilities of a Composite Slab for an Advanced Heat-sink Design written by Paul A. Libby and published by . This book was released on 1961 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Helium: Bibliography of Technical and Scientific Literature, 1962 by : Philip Cochran Tully
Download or read book Helium: Bibliography of Technical and Scientific Literature, 1962 written by Philip Cochran Tully and published by . This book was released on 1969 with total page 380 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Optimum Shape for Transpiration-cooled Nosetip of a Re-entry Vehicle by : Kevin E. Yelmgren
Download or read book Optimum Shape for Transpiration-cooled Nosetip of a Re-entry Vehicle written by Kevin E. Yelmgren and published by . This book was released on 1978 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: The variations of parameters method was used to determine the optimum nose shape for a reentry vehicle having a transpiration-cooled nosetip (TCNT). Three families of nose shapes were considered - The oblate ellipsoid, the flat face - round shoulder, and the spherical arc - round shoulder. These families are bounded by the flat face - sharp corner at one extreme and the hemisphere at the other extreme. The amount of coolant required by each nose shape during reentry was determined by using a high speed computer to couple the aerodynamic equations with the trajectory equations. The optimum shape is the shape which requires the least amount of coolant for reentry. The flat face - sharp corner shape was found to require the least amount of coolant, about 60 percent less water than the hemisphere. Although the time to impact is longer for the flat face, the smaller surface area and lower heating intensity more than offsets the increased reentry time. The possibility of an optimum flat face height was also investigated; no face height was found that minimized the total heating to the vehicle during reentry. (Author).
Download or read book Bibliographic Index written by and published by . This book was released on 1966 with total page 792 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis International Aerospace Abstracts by :
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1970 with total page 1064 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Report by : Tōkyō Daigaku. Kōkū Kenkyūjo
Download or read book Report written by Tōkyō Daigaku. Kōkū Kenkyūjo and published by . This book was released on 1971 with total page 530 pages. Available in PDF, EPUB and Kindle. Book excerpt:
