Evaluation of Blended Wing-body Combinations with Curved Plan Forms at Mach Numbers Up to 3.50
Author | : George H. Holdaway |
Publisher | : |
Total Pages | : 70 |
Release | : 1960 |
Genre | : Aerodynamics |
ISBN | : |
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Author | : George H. Holdaway |
Publisher | : |
Total Pages | : 70 |
Release | : 1960 |
Genre | : Aerodynamics |
ISBN | : |
Author | : George H. Holdaway |
Publisher | : |
Total Pages | : 82 |
Release | : 1960 |
Genre | : Aerodynamics |
ISBN | : |
Author | : George H. Holdaway |
Publisher | : |
Total Pages | : 80 |
Release | : 1961 |
Genre | : Aerodynamics |
ISBN | : |
Author | : Library of Congress Science and Technology Division |
Publisher | : |
Total Pages | : 252 |
Release | : 1962 |
Genre | : Aeronautics |
ISBN | : |
Author | : W. F. Lindsey |
Publisher | : |
Total Pages | : 24 |
Release | : 1954 |
Genre | : Aerodynamics |
ISBN | : |
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.