A Supersonic area rule and an application to the design of a wing-body combination with high lift-drag ratios /
As an extension of the transonic area rule, a concept for interrelating the wave drags of wing-body combinations at moderate supersonic speeds with axial developments of cross-sectional area has been derived. The wave drag of a combination at a given supersonic speed is related to a number of develo...
| Main Author: | |
|---|---|
| Corporate Authors: | , |
| Other Authors: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, DC :
U.S. G.P.O.,
1960.
|
| Series: | NASA TR ;
R-72 |
| Subjects: |