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 | : |
Evaluation Of Blended Wing Body Combinations With Curved Plan Forms At Mach Numbers Up To 350
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Investigation at Mach Numbers of 0.20 to 3.50 of Blended Wing-body Combinations of Sonic Design with Diamond, Delta and Arrow Plan Forms
| Author | : George H. Holdaway |
| Publisher | : |
| Total Pages | : 82 |
| Release | : 1960 |
| Genre | : Aerodynamics |
| ISBN | : |
Investigation at Mach Numbers of 0.60 to 3.50 of Blended Wing-body Combinations with Cambered and Twisted Wings with Diamond, Delta and Arrow Plan Forms
| Author | : George H. Holdaway |
| Publisher | : |
| Total Pages | : 80 |
| Release | : 1961 |
| Genre | : Aerodynamics |
| ISBN | : |
The Flow Past a Straight- and a Swept-wing-body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1.0
| 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.
