Flow Past A Straight And A Swept Wing Body Combination And Their Equivalent Bodies Of Revolution At Mach Numbers Near 10
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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.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 508 |
Release | : 1954 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 60 |
Release | : 1956 |
Genre | : Science |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 1056 |
Release | : 1972 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 1534 |
Release | : 1965 |
Genre | : Aeronautics |
ISBN | : |
Author | : Langley Aeronautical Laboratory |
Publisher | : Hassell Street Press |
Total Pages | : 26 |
Release | : 2021-09-09 |
Genre | : |
ISBN | : 9781014490469 |
This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it. This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Author | : |
Publisher | : |
Total Pages | : 1174 |
Release | : 1956 |
Genre | : Research |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 886 |
Release | : 1959 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 768 |
Release | : 1985 |
Genre | : Aeronautics |
ISBN | : |
Author | : Michael E. Tauber |
Publisher | : |
Total Pages | : 44 |
Release | : 1989 |
Genre | : Aerodynamic heating |
ISBN | : |