Screen LibraryIdealized wings and wing-bodies at a Mach number of 3 /
The purpose of this paper is to describe the theoretical possibilities for obtaining high lift-drag ratios at M = 3 and to describe some experiments which were designed to exploit the theory. In discussing the theoretical maximum lift-drag ratios of idealized arrangements, it is convenient to consid...
Saved in:
| Main Authors: | |
|---|---|
| Corporate Authors: | |
| Published: |
|
| Literature type: | Book |
| Language: | English |
| Series: |
Technical note / National Advisory Committee for Aeronautics ;
4361 |
| Subjects: | |
| Summary: |
The purpose of this paper is to describe the theoretical possibilities for obtaining high lift-drag ratios at M = 3 and to describe some experiments which were designed to exploit the theory. In discussing the theoretical maximum lift-drag ratios of idealized arrangements, it is convenient to consider, as a standard of comparison, the lifting flat plate. |
| Item Description: | NACA TN No. 4361. |
| Carrier Form: | 11 p. : ill. ; 27 cm. |
| Bibliography: | Includes bibliographical references. |
| CLC: | V211.41 |
| Call Number: | V211.41/K199 |