Download or read book Base flow Aerodynamics of a Saturn type Booster Stage at Mach Numbers 0 1 to 2 0 written by John L. Allen and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Basic Aerodynamics written by Gary A. Flandro and published by Cambridge University Press. This book was released on 2011-11-14 with total page 433 pages. Available in PDF, EPUB and Kindle. Book excerpt: In the rapidly advancing field of flight aerodynamics, it is especially important for students to master the fundamentals. This text, written by renowned experts, clearly presents the basic concepts of underlying aerodynamic prediction methodology. These concepts are closely linked to physical principles so that they are more readily retained and their limits of applicability are fully appreciated. Ultimately, this will provide students with the necessary tools to confidently approach and solve practical flight vehicle design problems of current and future interest. This book is designed for use in courses on aerodynamics at an advanced undergraduate or graduate level. A comprehensive set of exercise problems is included at the end of each chapter.
Download or read book Foundations of Aerodynamics written by Arnold M. Kuethe and published by . This book was released on 1986 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt: This is a revision of leading textboook for introductory courses in aerodynamics for junior/senior engineering students. Updated to include more extensive use of vectors, contemporary forwardswept and oblique-wing design concepts, expanded coverage of boundary layer control, additional problems, and extensive photographs to illustrate fluid flow concepts.
Download or read book Base flow Aerodynamics of a Saturn type Booster Stage at Mach Numbers 0 1 to 2 0 written by John L. Allen and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Computational Fluid Dynamics of the Base Flow on a Plane Body Between a Subsonic Flow on One Side and a Supersonic Flow on the Other written by Mohammad J. Izadi and published by . This book was released on 1991 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Study of Axially symmetric Subsonic Base Flow written by Robert Gerald VanWagenen and published by . This book was released on 1968 with total page 530 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Separated and Vortical Flow in Aircraft Wing Aerodynamics written by Ernst Heinrich Hirschel and published by Springer Nature. This book was released on 2020-10-04 with total page 458 pages. Available in PDF, EPUB and Kindle. Book excerpt: Fluid mechanical aspects of separated and vortical flow in aircraft wing aerodynamics are treated. The focus is on two wing classes: (1) large aspect-ratio wings and (2) small aspect-ratio delta-type wings. Aerodynamic design issues in general are not dealt with. Discrete numerical simulation methods play a progressively larger role in aircraft design and development. Accordingly, in the introduction to the book the different mathematical models are considered, which underlie the aerodynamic computation methods (panel methods, RANS and scale-resolving methods). Special methods are the Euler methods, which as rather inexpensive methods embrace compressibility effects and also permit to describe lifting-wing flow. The concept of the kinematically active and inactive vorticity content of shear layers gives insight into many flow phenomena, but also, with the second break of symmetry---the first one is due to the Kutta condition---an explanation of lifting-wing flow fields. The prerequisite is an extended definition of separation: “flow-off separation” at sharp trailing edges of class (1) wings and at sharp leading edges of class (2) wings. The vorticity-content concept, with a compatibility condition for flow-off separation at sharp edges, permits to understand the properties of the evolving trailing vortex layer and the resulting pair of trailing vortices of class (1) wings. The concept also shows that Euler methods at sharp delta or strake leading edges of class (2) wings can give reliable results. Three main topics are treated: 1) Basic Principles are considered first: boundary-layer flow, vortex theory, the vorticity content of shear layers, Euler solutions for lifting wings, the Kutta condition in reality and the topology of skin-friction and velocity fields. 2) Unit Problems treat isolated flow phenomena of the two wing classes. Capabilities of panel and Euler methods are investigated. One Unit Problem is the flow past the wing of the NASA Common Research Model. Other Unit Problems concern the lee-side vortex system appearing at the Vortex-Flow Experiment 1 and 2 sharp- and blunt-edged delta configurations, at a delta wing with partly round leading edges, and also at the Blunt Delta Wing at hypersonic speed. 3) Selected Flow Problems of the two wing classes. In short sections practical design problems are discussed. The treatment of flow past fuselages, although desirable, was not possible in the frame of this book.
Download or read book Foundations of Aerodynamics written by Arnold Martin Kuethe and published by John Wiley & Sons. This book was released on 1976 with total page 552 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Effect of Bleed of Two dimensional Base Flow at Subsonic Transonic and Low Supersonic Speeds written by N. Pollock and published by . This book was released on 1978 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt: Measurements of the effect of bleed on the base pressure acting on a two-dimensional blunt trailing edge aerofoil are reported and schlieren photographs of the base flow are presented. The tests covered a Mach number range of 0.5 to 1.35 at a base height Reynolds number of approximately 90,000 with turbulent approach boundary layers. The results indicate that small bleed quantities can produce considerably greater base drag reductions at transonic speeds than at subsonic or supersonic speeds. A bleed mass flow coefficient of 0.07 produces a lower base drag than the best practical non-bleed blunt trailing edge geometry through the entire test Mach number range. (Author).
Download or read book Experimental Investigation of Stage Separation Aerodynamics written by Robert A. Wasko and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Hydro and Aeromechanics written by Oskar Karl Gustav Tietjens and published by Courier Corporation. This book was released on 1957-01-01 with total page 338 pages. Available in PDF, EPUB and Kindle. Book excerpt: Prandtl was one of the great theorists of aerodynamics and this work has long been considered one of the finest introductory works in the field. Topics include flow through pipes, Prandtl's own work on boundary layers, drag, airfoil theory, and entry conditions for flow in a pipe.
Download or read book An Empirically Derived Basis for Calculating the Area Rate and Distribution of Water drop Impingement on Airfoils written by Antonio Ferri and published by . This book was released on 1952 with total page 346 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Base Flow and Exhaust Plume Interaction written by M. M. J. Schoones and published by . This book was released on 1998 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Computation of the Base Flow for an Axi symmetric Nacelle Configuration written by Doo Sung Baik and published by . This book was released on 1997 with total page 240 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Basic Aerodynamic Noise Research written by Ira R. Schwartz and published by . This book was released on 1969 with total page 548 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Unified Theoretical Foundations of Lift and Drag in Viscous and Compressible External Flows written by Luo-Qin Liu and published by Springer. This book was released on 2017-09-29 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt: This thesis analyzes aerodynamic forces in viscous and compressible external flows. It is unique, as the force theories discussed apply to fully viscous and compressible Navier-Stokes external flows, allowing them to be readily combined with computational fluid dynamics to form a profound basis of modern aerodynamics. This thesis makes three fundamental contributions to theoretical aerodynamics, presenting: (1) a universal far-field zonal structure that determines how disturbance flow quantities decay dynamically to the state of rest at infinity; (2) a universal and exact total-force formula for steady flow and its far-field asymptotics; and (3) a general near-field theory for the detailed diagnosis of all physical constituents of aerodynamic force and moment.
Download or read book Aerodynamics of Base Combustion written by S. N. B. Murthy and published by . This book was released on 1976 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt:
