File:X-15 Configurations (LRC-1958-B701 P-01966).tiff
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Summary
[edit]DescriptionX-15 Configurations (LRC-1958-B701 P-01966).tiff |
English: This scale-model of North American's initial X-15 design was tested in North American and NACA wind tunnels note the conventional tail and fuselage side-tunnels that extend far toward the aircraft nose. North American engineers would determine that the variable wedge-angle stabilizer created a weight issue, and aeronautical testing by Langley engineers confirmed that the side-tunnels made the design less stable. |
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Date | Taken on 6 May 1958 | ||
Source |
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Author | NASA Langley Research Center / NACA | ||
Keywords InfoField | X-15; North American; NASA; LARC; 1958-L-01966; Langley; LRC; LRC-1958-B701_P-01966 |
Licensing
[edit]Public domainPublic domainfalsefalse |
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This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.) | ![]() |
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Image title | This scale-model of North American's initial X-15 design was tested in North American and NACA wind tunnels note the conventional tail and fuselage side-tunnels that extend far toward the aircraft nose. North American engineers would determine that the variable wedge-angle stabilizer created a weight issue, and aeronautical testing by Langley engineers confirmed that the side-tunnels made the design less stable. |
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Author | NACA |
Width | 3,818 px |
Height | 2,516 px |
Bits per component | 8 |
Compression scheme | LZW |
Pixel composition | Black and white (Black is 0) |
Orientation | Normal |
Number of components | 1 |
Number of rows per strip | 68 |
Horizontal resolution | 400 dpi |
Vertical resolution | 400 dpi |
Software used | Adobe Photoshop CS5 Macintosh |
File change date and time | 13:17, 10 January 2012 |
Color space | Uncalibrated |