The Flow Past a Straight- and a Swept-wing-body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1.0 PDF Download
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Author: W. F. Lindsey Publisher: ISBN: Category : Aerodynamics Languages : en Pages : 24
Book Description
Abstract: The complete flow fields past a straight and a swept wing-body combination and their equivalent bodies of revolution at Mach numbers around 1.0 have been observed by means of motion-picture schlieren photography. The results of these observations indicate that the shock growth and positions on the wing-body combinations are closely reproduced in the flow past their respective equivalent bodies.
Author: W. F. Lindsey Publisher: ISBN: Category : Aerodynamics Languages : en Pages : 24
Book Description
Abstract: The complete flow fields past a straight and a swept wing-body combination and their equivalent bodies of revolution at Mach numbers around 1.0 have been observed by means of motion-picture schlieren photography. The results of these observations indicate that the shock growth and positions on the wing-body combinations are closely reproduced in the flow past their respective equivalent bodies.
Author: Holt Ashley Publisher: Courier Corporation ISBN: 0486648990 Category : Technology & Engineering Languages : en Pages : 306
Book Description
This excellent, innovative reference offers a wealth of useful information and a solid background in the fundamentals of aerodynamics. Fluid mechanics, constant density inviscid flow, singular perturbation problems, viscosity, thin-wing and slender body theories, drag minimalization, and other essentials are addressed in a lively, literate manner and accompanied by diagrams.
Author: W. F. Lindsey
Author: W. F. Lindsey
Author: United States. National Advisory Committee for Aeronautics
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Author: Michael E. Tauber
Author: Holt Ashley