Tests of Aerodynamically Heated Multiweb Wing Structures in a Free Jet at Mach Number 2: Four Aluminum-Alloy Models of 20-Inch Chord and Span With 0.064-Inch-Thick Skin, 0.025-Inch-Thick Ribs and Webs, and Zero, One, Two, or Three Chordwise Ribs
| Author: | Davidson, John R. |
|---|---|
| Additional Authors: | Rosecrans, Richard |
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L57L13 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc63901/ |