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Lift and pitching-moment interference between a pointed cylindrical body and triangular wings of various aspect ratios at mach numbers of 1.50 and 2.02
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1956 |
| Description | The lift and pitching-moment characteristics of a body alone, six triangular wings of various aspect ratios, and the combinations were measured at Mach numbers of 1.50 and 2.02 at a Reynolds number of 5.5 million (based on the body length) for angles of attack up to 5.5 degrees. The total lift and pitching-moment interference were determined and compared with theory. The agreement was found to be good. |
| File Size | 23271755 |
| Page Count | 52 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930084523 |
| Archival Resource Key | ark:/13960/t48q0r78q |
| Language | English |
| Publisher Date | 1956-12-01 |
| Access Restriction | Open |
| Subject Keyword | Research Technique - Corrections Wings, Complete - Aspect Ratio Wing-body Combinations - Missiles Bodies Wing-fuselage Combinations - Airplanes Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |