Download or read book Hypersonic Flow Near the Leading Edge of a Flat Plate written by Henry T. Nagamatsu and published by . This book was released on 1960 with total page 2 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effect of Leading edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5 7 written by Marcus O. Creager and published by . This book was released on 1960 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Leading Edge Effect on Rarefied Hypersonic Flow Over a Flat Plate written by K. S. Heffner and published by . This book was released on 1991 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Critical Assessment of the Problem of Sharp Leading Edge of a Flat Plate in Hypersonic Flow written by Amolak C. Jain and published by . This book was released on 1964 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: The advent of vehicles, moving many times the velocity of sound makes it necessary to understand clearly the various phenomena occuring near the sharp leading edge of a flat plate. A few theoretical attempts to tackle this problem are made and several experiments are performed at various places. Unfortunately wide areas of disagree ment exist between the various theoretical investigations and experimental results. It is the purpose of the note to try to gather some useful information from the available literature on this subject and present some suggestions which might be useful or worth consideration in any future attempt of solving this problem. (Author).

Download or read book Effect of Leading edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5 7 written by Marcus O. Creager and published by . This book was released on 1960 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Kinetic Study of the Hypersonic Flow Past the Leading Edge of a Flat Plate written by Rateb Jaber El Assar and published by . This book was released on 1968 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Kinetic Study of the Hypersonic Flow Past the Leading Edge of a Flat Plate written by R. J. El-Assar and published by . This book was released on 1970 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book On the Hypersonic Sharp Leading Edge Problem for Bodies Other Than Flat Plates written by Jay M. Solomon and published by . This book was released on 1965 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The flow near the tip of pointed nosed bodies in hypersonic flight is considered. In particular, the region where continuum concepts are applicable, but where boundary layer theory is no longer valid, is studied using the model proposed by Oguchi for the flat plate problem. Both two-dimensional and axiallysymmetric bodies are considered. Solutions are obtained in the form of expansions valid near the nose tip. The surface pressure is found to approach a finite value as the tip is approached; numerical results for this limit value are obtained for various wall to total temperature ratios and tip semi-vertex angles. (Author).

Download or read book Effect of Slight Blunting of Leading Edge of an Immersed Body on the Flow Around it at Hypersonic Speeds written by Goromir Goromirovich Chernyĭ and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Leading edge Effects on the Laminar Flat plate Boundary Layer and the Aerodynamic Heating at Mach 10 4 written by Howard W. Stone and published by . This book was released on 1969 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Studies of the Leading Edge Effect on the Rarefied Hypersonic Flow Over a Flat Plate written by William Whyte Joss and published by . This book was released on 1968 with total page 7 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Local Leading Edge Heat Transfer on a Flat Plate in Rarefied Hypersonic Flow written by James David Hendry and published by . This book was released on 1964 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: The local heat flux to a sharp edged flat plate was measured over the range 32.8

Download or read book Hypersonic Slip Flow Past the Leading Edge of a Cooled Flat Plate written by W. L. Chow and published by . This book was released on 1966 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book On the Hypersonic Flow Over a Delta Wing with Very Supersonic Leading Edges written by Norman D. Malmuth and published by . This book was released on 1965 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Shock Wave and Viscous Layer Structure in a Rarefied Hypersonic Flow Near the Leading Edge of a Sharp Flat Plate written by and published by . This book was released on 1967 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Sharp Leading Edge Problem in Hypersonic Flow written by Hakuro Oguchi and published by . This book was released on 1960 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt: In the present paper the problem of hypersonic viscous flow past a semi-infinite flat plate with a sharp leading edge is considered. The study is concerned primarily with the rarefied flow region close enough to the leading edge that there is no longer an inviscid layer but where the shock wave is still thin. The solution which is obtained is shown to approach a wedge-like flow near the leading edge with a straight induced shock wave.

Download or read book Theoretical Analysis of Near free molecule Hypersonic Flow at the Sharp Leading Edge of a Flat Plate written by A. F. Charwat and published by . This book was released on 1963 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: The initial interactions between a hypersonic free stream and molecules emitted (reflected diffusely) by a cold flat plate immediately downstream of its sharp leading edge are analyzed by near-free-molecule theory. The results give the variations of the pressure, shear, and heat transfer at the wall. These are found to in crease downstream from the leading edge and reach a maximum plateau, and a subsequent decay of the wall-transfer properties to continuum boundary-layer values can be inferred. The magnitude and location of this plateau compare well with available viscous pressure interaction data. An indication of the initial growth rate of the disturbed merged layer is also obtained from the analysis. It is found that this region is wedgelike and has a slope of approximately 45 deg for all hypersonic Mach numbers and for wall to- free-stream-temperature ratios of the order of unit.