20040034216 · A Theoretical Investigation of the Drag of Generalized Aircraft Configurations in Supersonic Flow
NASA · 1957
Overview
It seems possible that, in supersonic flight, unconventional arrangements of wings and bodies may offer advantages in the form of drag reduction. It is the purpose of this report to consider the methods for determining the pressure drag for such unconventional configurations, and to consider a few…
Source & rights
Source: ntrs.nasa.gov. Public-domain U.S. Government work (17 USC §105) — freely reproducible.
Permanent URL — we don’t break links.
Document details
- Doc number ·
- 20040034216
- Publisher ·
- NASA
- Year ·
- 1957
- File size ·
- 3.8 MB