Author: Clark H. Lewis Publisher: ISBN: Category : Aerodynamics, Hypersonic Languages : en Pages : 182
Book Description
Contents: A survey of higher-order boundary-layer theory; Finite difference solution of the first-order boundary-layer equations; Laminar boundary-layer calculations on bodies of revolution in hypersonic flow; Solution of the viscous shock-layer equations for a binary mixture; Viscous shock-layer problem for the stagnation point of a blunt body; Chemically reacting boundary layer effects for the agard engineering applications body and flow conditions; Computation of higher-order boundary-layer effects with a first-order treatment and comparison with experimental data; Higher-order boundary-layer effects for the agard engineering applications body and flow conditions; The hypersonic viscous shock-layer problem; Numerical methods for nonreacting and chemically reacting laminar flows - tests and comparisons.
Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development Publisher: ISBN: Category : Languages : un Pages :
Author: William H. Dorrance Publisher: Courier Dover Publications ISBN: 0486822583 Category : Technology & Engineering Languages : en Pages : 353
Book Description
Designed for advanced undergraduate and graduate courses in modern boundary-layer theory, this frequently cited work offers a self-contained treatment of theories for treating laminar and turbulent boundary layers of reacting gas mixtures. 1962 edition.
Author: E. Clay Anderson Publisher: ISBN: Category : Chemical equilibrium Languages : en Pages : 180
Book Description
Turbulent boundary layer flows of non-reacting gases are predicted for both interal (nozzle) and external flows. Effects of favorable pressure gradients on two eddy viscosity models were studied in rocket and hypervelocity wind tunnel flows. Nozzle flows of equilibrium air with stagnation temperatures up to 10,000 K were computed. Predictions of equilibrium nitrogen flows through hypervelocity nozzles were compared with experimental data. A slender spherically blunted cone was studied at 70,000 ft altitude and 19,000 ft/sec. in the earth's atmosphere. Comparisons with available experimental data showed good agreement. A computer program was developed and fully documented during this investigation for use by interested individuals.
Author: John David Anderson Publisher: AIAA ISBN: 9781563474590 Category : Science Languages : en Pages : 710
Book Description
This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development Publisher: ISBN: Category : Aeronautics Languages : en Pages : 600
Author: Clark H. Lewis
Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development
Author: Clark H. Lewis
Author: 
Author: William H. Dorrance
Author: E. Clay Anderson
Author: John David Anderson
Author: U. Müller
Author: 
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development